MS-364, BERNARD LINDENBAUM VERTICAL FLIGHT RESEARCH COLLECTION

Collection Number: MS-364

Title: Bernard Lindenbaum Vertical Flight Research Collection

Dates: 1918-1999 (Bulk 1945-1980)

Creator: Lindenbaum, Bernard, 1916-2002

Summary/Abstract: Bernard Lindenbaum was an aeronautical engineer with the Air Force Flight Dynamics Laboratory (AFFDL) at Wright-Patterson Air Force Base in Dayton, Ohio from the mid-1940s until the mid-1970s. During his time with the laboratory, he was involved in the research and development of many types of vertical take-off and landing aircraft (VTOL) including the Avro “Avrocar,” a number of Sikorsky helicopters, the Vought XC-142 tilt wing, and many other similar aircraft. His collection of vertical flight research material contains numerous technical reports chronicling the development of military helicopters and V/STOL aircraft, a variety of conference reports and notes, many NACA/NASA technical notes, blueprints of several V/TOL aircraft, 190 reels of 16mm film and 10 VHS tapes of helicopter and V/STOL testing.

Quantity/Physical Description: 126.3 linear feet

Language(s): English

Repository: Special Collections and Archives, Paul Laurence Dunbar Library, Wright State University, Dayton, OH 45435-001, (937) 775-2092

Restrictions on Access: There are no restrictions on accessing material in this collection.

Restrictions on Use: Copyright restrictions may apply. Unpublished manuscripts are protected by copyright. Permission to publish, quote or reproduce must be secured from the repository and the copyright holder.

Preferred Citation: (Box Number, Folder Number), MS-364, Bernard Lindenbaum Vertical Flight Research Collection, Special Collections and Archives, University Libraries, Wright State University, Dayton, Ohio

Acquisition: The collection was donated by Stephen Lindenbaum of Marietta, Georgia, son of Bernard Lindenbaum, on March 24, 2003.

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Separated Material: Aviation books and Vertiflight Magazine, received with the collection, have been cataloged and placed on the shelves in the Special Collection and Archives Reading Room.

16 mm film contained in the collection is located in the Special Collections and Archives Film vault located in the basement of the Wright State University Medical Sciences Building. Researchers should call in advance to view the film.

Additional Sources: Lindenbaum, Bernard, “V/STOL Concepts and Developed Aircraft, Volume I: A Historical Report (1940-1986), Universal Energy Systems, Inc., Dayton, Ohio, Report Number A973571, 26 Jun 1986.

Processing Information: This collection has been minimally processed and minimally organized. Each box has been fully inventoried and a list of items included in the container listing. No effort was made to replace folders with acid-free folders and reports remain in their original cover.

Processed by: Ed O’Shaughnessy (Archives Volunteer) and John Armstrong, 2010-2011.

Arrangement: The collection is arranged in twelve series.

Series I: Rotary Wing Handbook Series II: NACA & NASA Reports Series III: AVRO Avrocar Series IV: Helicopters Series V: Helicopter Aerodynamics Series VI: Convertiplane, Autogiro, Composite Research Vehicle and Stowed Rotor Series VII: SR-175, Tri-Service Transport and V/STOL Transports Series VIII: Vertical Lift Theory and Aerodynamics – Non-Helicopter Series IX: Escape Systems, Crash and Rescue Series X: Power Plants, Propellers, RPV, Drone, Small Tactical Aerial Vehicle, and STAMP Series XI: Microfilm Series XII: Film

Biographical/Historical Note: Bernard Lindenbaum was born in 1916. In 1943 he was appointed a de la Cierva Fellow at New York University’s College of Engineering. In 1944 he received his Master of Aeronautical Engineering.

Lindenbaum has held a variety of positions during his engineering career ranging from Junior Aeronautical Engineer to Deputy for Analysis in the V/STOL Technology Division of the Flight Dynamics Laboratory. Some of the projects he participated in include: Sikorsky R-5, Kellett XR-8 “Synchropter,” Firestone XT9 A&B, Kellett XR-10 Synchropter transport, Bell XR-12 utility and light transport, Firestone XR-14 twin tail rotor helicopter, Piasecki XH-16 tandem

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rotor transport, Hughes XH-17 pressure jet rotor helicopter, Sikorsky H-19 light transport, Piasecki H-21 Artic Rescue, American H-26 pulse jet driven rotor, Bell H-40 (renamed UH-1), Kaman H-43 local base rescue, Bell XV-3 tilt rotor, Hiller X-18 tilt wing, Curtiss-Wright X-19 tilt propeller, Vought XC-142 tilt wing, AVRO “Avrocar,” Hawker P-1127, and others.

Lindenbaum retired from the United States Air Force in 1974. He served on the National Advisory Committee for Aeronautics (NACA) Helicopter Subcommittee and was a U.S. Data Exchange Officer on V/STOL Aircraft with the Federal Republic of Germany and France. He authored the definitive Volume 1 of V/STOL Concepts and Developed Aircraft for the U.S. Air Force and Navy.

Lindenbaum is a founding member of the American Helicopter Society (AHS) and a member of the society since 1945. He participated on the AHS Board of Directors as a Midwest Vice President. In 1970 he was awarded an AHS Honorary Fellowship and in 1974 he was chosen to receive the Society’s highest honor, the Alexander Klemin Award.

Bernard Lindenbaum died in 2002.

Scope and Content: The Bernard Lindenbaum Vertical Flight Research Collection is a very large collection documenting the history and development of helicopters and V/STOL aircraft from the mid­1940s to the 1990s. The collection contains research reports, conference reports, blueprints, and film documenting this development. Researchers should be aware that the collection was minimally processed in that each box was fully inventoried, but no effort was made to place the material in acid-free folders, number folders, or relocate similar material together. As a result, some boxes will have more than one-topic and the same reports may appear in multiple boxes in the same series or under different series. When researching the collection, researchers should look through all of the boxes with similar headings to locate material. The collection has been organized into twelve, broad series topics.

Series I, Rotary Wing Handbook, consists of one Record Center box containing eight of the eighteen volumes of the Rotary Wing Handbook. The series also contains Part I and II of the 1960 Russian book “The Aerodynamic Design of Helicopters.”

Series II, NACA & NASA Reports, consists of five Record Center boxes containing National Advisory Committee on Aeronautics (NACA), and its successor, the National Aeronautics and Space Administration (NASA), reports on helicopters, V/STOL aircraft, VTOL aircraft, air foils, and tilted rotors. The date span for the reports is 1929 to 1977. There are also NACA annual reports from 1934 to 1941 and the proceedings of V/STOL Technology and Planning Conference held September 23 to 25, 1969.

Series III, AVRO Avrocar, consists of three Record Center boxes containing reports, progress reports, and photographs on the development of the Avrocar. The reports span a period beginning in 1958 and ending in 1990. There is also film of the Avrocar in Series XII.

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Series IV, Helicopters, is a fairly large series consisting of eight Record Center boxes containing reports spanning a period from1934 to 1997. The series includes early, pre-1960 reports on helicopters, blueprints of Kellett and Piasecki aircraft, and helicopter history articles and photographs. The series also contains helicopter brochures and information on early helicopters and towed helicopters.

Series V, Helicopter Aerodynamics, is a large series consisting of twenty Record Center boxes documenting helicopter aerodynamics from 1918 to 1993. The series includes reports on: helicopter dynamics, performance, and theory; rotors, rotor blades, and rotor aerodynamics; rotor blade test and helicopter controls; helicopter airfoils; helicopter vibration; aerial utility vehicles; hot cycle rotors and wing composite aircraft; and aerodynamics and the Kaman Model K-190. The series also contains American Helicopter Society Forum Reports from the 1970s and reports from the 1980 Propeller Propulsion Conference.

Series VI, Convertiplane, Autogiro, Composite Research Vehicle and Stowed Rotor, is another large series consisting of seventeen Record Center boxes containing reports from 1923 to 1999. This series contains reports on: the Convertiplane Model XV-1; stoppable and stowed rotors; convertiplane composite research aircraft; autogiros; compound helicopters; autogiro gliders and kites; tip-mounted power; and compound and rigid rotor helicopters.

Series VII, SR-175, Tri-Service Transport and V/STOL Transports, consists of nineteen Record Center boxes containing reports from 1938 to 1990. The topic of these reports center on tri­service and V/STOL transports. Included in this series are reports from the 1st National V/STOL Aircraft Symposium held November 3-4, 1965. The series also includes a wide-variety of other topics including: the Bell SR-175 and ducted propellers; the tilt-wing propelloplane; lift fans and fans in wings; V/STOL short-haul transports; the Bell X-22A program, and reports on tilt wing V/STOL aircraft including the CL-84, X-18, VC-400, and XC-142A. The series also contains reports from the Academic VTOL and American Helicopter Society Proceedings and the First Convertible Aircraft Proceedings, and American Helicopter Society Forum reports from 1947 to 1972.

Series VIII, Vertical Lift Theory and Aerodynamics – Non-Helicopter, is one of the largest series in the collection spanning twenty-five Records Center boxes. The reports span a period from 1932 to 1989. Included in this series are reports on: tri-service transports, the Harrier; V/STOL propeller technology concepts; lift-fan flight research; high-lift devices; V/TOL and GETOL ground effects; tilt-wing aircraft; downwash and ground effects; shrouded propellers and propulsion systems; stopped rotor compound helicopters; and ducted and shrouded propellers.

Series IX, Escape Systems, Crash and Rescue, is a small series consisting of three Record Center boxes. This series includes reports from 1929 to 1999 that include information on escape systems and crash rescue helicopters.

Series X, Power Plants, Propellers, RPV, Drone, Small Tactical Aerial Vehicle, and STAMP, is another small series consisting of four Record Center boxes. The series includes information on: drone aircraft; remotely piloted vehicles; power plants; propellers; and the Small tactical Aerial Mobility Platform (STAMP). The series also contains reports from the Conference on Propeller

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Propulsion held April 22-24, 1980 and a copy of Lindenbaum’s presentation on “V/STOL Concepts and Developed Aircraft: A Historical Review.”

Series XI, Microfilm, is located in one box (Box 106) and includes the records of the Prewitt Aircraft Company, Clifton Heights, Pennsylvania. The microfilm contains reports on the history of the helicopter and rotary wing aircraft history.

Series XII, Film, consists of 190 reels of 16 mm film and 10 VHS cassettes documenting vertical flight reports and history from 1938 to 1977. Some of the film is in poor condition and all need to be converted to a VHS or DVD format for viewing. The series includes film of the XC-4B Hummingbird, the Bell XC-142, and the AVRO Avrocar, plus film of many other vertical flight aircraft.

Subject Terms

Persons/Families Lindenbaum, Bernard, 1916-2002

Organizations/Corporate Names Air Force Flight Dynamics Laboratory (U.S.)

Places Dayton (Ohio) Wright-Patterson Air Force Base (Dayton, Ohio)

Subjects (General) V/STOL Technology and Planning Conference (1969: Las Vegas, Nev.) Helicopters

Convertiplanes Jet helicopters Military helicopters Rotors (Helicopters) Sikorsky helicopters

Helicopters - - Aerodynamics Vertical rising aircraft Tilt rotor aircraft Avrocar (VTOL airplane)

Material Types Technical reports Blueprints Film Books Photographs Microfilm

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Occupations Aeronautical Engineer

Collection Inventory

SERIES I: Rotary Wing Handbook, 1943-1969

Box File Description Date

1 1 Volume 9 of 18: Rotor Blade Handbook Contract No. W33-038 ac-21804 (20695)

1958

2 Volume 5 of 18: Rotor Wing Handbook, Weight and Balance PB 121097

1954

3 Volume 6 of 18: Rotor Wing Handbook, Aerodynamics and Performance of Helicopters PB111390

1954

4 Volume 7 of 18: Rotary Wing Handbook, Vibrations Handbook for Helicopters 111289

1954

5 Volume 10 of 18: Rotary Wing Handbook, Stability and Control of Rotary Wing Aircraft PB111521

1954

6 Volume 11 of 18: Rotary Wing Handbook, Special Types of Rotary Wing Aircraft PB111633

1954

7 Volume 13 of 18 Rotary Wing Handbook– Convertible Aircraft Contract# W33-038 ac-21804 (20695)

1954

8 Volume 14 of 18: Rotary Wing Handbook, The Rotary Wing Industry PB111391

1954

9 Rotary Wing Handbook, Contractor’s Correspondence Project R-458-393 WCLSR 3

Jun 8 1954

10 Aerodynamic Investigations of Rotary Wing Configurations Project R458-393

1952-1954

11 General Investigations of Airplanes, Rotorcraft and Missile Stability + Control and Performance 1365-13541A

1950-1956

12 Early Rotary Wing Gliders, Pictures and Specifications 1943-1948 13 Rotary Wing Aircraft Handbook, Correspondence 1956 14 Wind Tunnel Tests on XR-10 Helicopter Model Volume I Mar1945 15 Wind Tunnel Tests on XR-10 Helicopter Model Volume II Apr 1945 16 A Preview of 18 Volumes of the Rotary Wing Handbooks

and History Project May 10 1950

17 NASA TT F-494 Helicopters, Calculation and Design Volume 1 Aerodynamics

Sep 1967

18 FTD TT 62-815 Problems of the Aerodynamics of Helicopter Lifting Rotors

Oct 3 1962

19 FSTC-HT-23-549-71 Helicopter Aerodynamics USSR 1969 20 F-TS-9794/V The Aerodynamic Design of Helicopters Part

I USSR Apr 1960

21 F-TS-9794/V The Aerodynamic Design of Helicopters Part II USSR

Apr1960

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SERIES II: NACA & NASA Reports, 1929-1977

Box File Description Date

2 1 NASA TN D-243 Tables and Charts for Estimating Stall Effects on Lifting-Rotor Characteristics

May 1960

2 NASA TN D-317 Wind-Tunnel Tests of a Circular Wing with an Annular Nozzle in Proximity to the Ground

1960

3 NASA TN D-326 Large-Scale Wind Tunnel Tests of a Wingless Vertical Take-Off and Landing Aircraft – Preliminary Results

Jun 15 1960

4 NASA TN D-372 A Flight Study of the Conversion Maneuver of a Tilt-Duct VTOL Aircraft

Nov 1960

5 NASA TN D-376 High-Tip-Speed Static-Thrust Tests of a Rotor Having NACA 63(215)A018 Airfoil Sections with and without Vortex Generators Installed

May 1960

6 NASA TN D-382 Effect of Blade Cutout on Power Required by Helicopters Operating at High Tip-Speed Ratios

Sep 1960

7 NASA TN D-397 Data from a Static-Thrust Investigation of a Large Scale General Research VTOL-STOL Model in Ground Effect

Aug 1960

8 NASA TN D-444 Lateral Stability and Control Characteristics of a Four-Propeller Deflected-Slipstream VTOL Model Including the Effects of Ground Proximity

Jan 1961

9 NASA TN D-445 Investigation of Longitudinal and Lateral Stability Characteristics of a Six-Propeller Deflected-Slipstream VTOL Model with Boundary-Layer Control Including Effects of Ground Proximity

Jan 1961

10 NASA TN D-624 A Preliminary Study of V/STOL Transport Aircraft and Bibliography of NASA Research in the VTOL-STOL Field

Jan 1961

11 NASA TN D-658 Ground Influence on a Model Airfoil with a Jet-Augmented Flap as Determined by Two Techniques

Feb 1961

12 NASA TN D-730 Aerodynamic Characteristics of Propeller-Driven VTOL Aircraft

Mar 1961

13 NASA TN D-731 Induced Interference Effects on Jet and Buried-Fan VTOL Configurations in Transition

Mar 1961

14 NASA TN D-733 Review of Basic Principles of V/STOL Aerodynamics

Mar 1961

15 NASA TN D-736 Noise Considerations in the Design and Operation of V/STOL Aircraft

Apr 1961

16 NASA TN D-737 Some Recent Studies in Structural Dynamics of Rotor Aircraft

Mar 1961

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17 NASA TN D-774 Operational Technique for Transition of Several Types of V/STOL Aircraft

Mar 1961

18 NASA TN D-775 Aerodynamic Characteristics of a Large-Scale Model with a High Disk-Loading Lifting Fan Mounted in the Fuselage

Jul 25 1961

19 NASA TN D-776 A Wind Tunnel Investigation of a 4­Foot-Diameter Ducted Fan Mounted on the Tip of a Semispan Wing

Feb 27 1961

20 NASA TN D-812 Effects of Gyroscopic Cross Coupling Between Pitch and Roll on the Handling Qualities of VTOL Aircraft

Apr 1961

21 NASA TN D-818 Method for Calculating Induced Velocities at the Blades of a Slightly Inclined Propeller with Constant Circulation

May 1961

22 NASA TN D-901 Aerodynamic Characteristics of a Four-Propeller Tilt-Wing VTOL Model with Twin Vertical Tails, Including Effects of Ground Proximity

Jun 1961

23 NASA TN D-920 Stability and Control Characteristics of a Small-Scale Model of an Aerial Vehicle Supported by Two Ducted fans

Aug 3 1961

24 NASA TN D-933 Tables of Interference Factors for Use in Wind-Tunnel and Ground-Effect Calculations for VTOL/STOL Aircraft Part I-Wind Tunnels Having Width-Height Ratio of 2.0

Jan 1962

25 NASA TN D-935 Tables of Interference Factors for Use in Wind-Tunnel and Ground-Effect Calculations for VTOL/STOL Aircraft Part III-Wind Tunnels having Width-Height Ratio of 1.0

Jan 1962

26 NASA TN D-936 Tables of Interference Factors for Use in Wind-Tunnel and Ground-Effect Calculations for VTOL/STOL Aircraft Part IV-Wind Tunnels having Width-Height Ratio of 0.5

Jan 1962

27 NASA TN D-937 Stability and Control Characteristics of a Model of an Aerial Vehicle Supported by Four Ducted Fans

Aug 1961

28 NASA TN D-970 Effect of Ground Proximity on the Aerodynamic Characteristics of Aspect-Ratio-1 Airfoils with and Without End Plates

Oct 1961

29 NASA TN D-973 Effects of Gyroscopic Cross Coupling Between Pitch and Yaw of the Handling Qualities of VTOL Aircraft

Nov 1961

30 NASA TN D-981 Aerodynamic Characteristics of a Powered Semispan Tilting-Shrouded-Propeller VTOL Model in Hovering and Transition Flight

Jan 1962

31 NASA TN D-989 Summary of Flight-Test Results of the VZ-2 Tilt-Wing Aircraft

Feb 1962

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32 NASA TN D-995 Aerodynamic Loads on an Isolated Shrouded-Propeller Configuration for Angles of Attack from -10 to +110 Degrees

Jan 1962

33 NASA TN D-996 An Analytical Trend Study of Propeller Whirl Instability

Apr 1962

34 NASA TN D-1032 STOL Characteristics of a Propeller-Driven Aspect-Ratio-10, Straight-Wing Airplane with Boundary-Layer Control Flaps, as Estimated from Large-Scale Wind-Tunnel Tests

Jun 1961

35 NASA TN D-1034 Large-Scale Wind-Tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ratio 5.5, and with Four Propellers and Blowing Flaps

Jun 1961

36 NASA TN D-1201 A Preliminary Piloted Simulator and Flight Study of Height Control Requirements for VTOL Aircraft

Feb 1962

37 NASA TN D-1234 Force-Test Investigation of a Model of an Aerial Vehicle Supported by Four Unshrouded Propellers

Apr 1962

38 NASA TN D-1235 Flight-Test Investigation of a Model of an Aerial Vehicle Supported by Four Unshrouded Propellers

Apr 1962

39 NASA TN D-1257 Division of Aerodynamic Loads on a Semispan Tilting-Ducted-Propeller Model in Hovering and Transition Flight

May 1962

40 NASA TN D-1272 Aerodynamic Characteristics in Pitch of Several Ring-Wing-Body Configurations at a Mach Number of 2.2

Apr 1962

41 NASA TN D-1301 Aerodynamic Characteristics of a 4­Foot-Diameter Ducted Fan Mounted on the Tip of a Semispan Wing

Apr 1962

42 NASA TN D-1382 Slipstream Flow Around Aeveral Tilt-Wing VTOL Aircraft Models Operating Near the Ground

Sep 1962

43 NASA TN D-1430 Longitudinal Trim Characteristics of a Deflected Slipstream V/STOL Aircraft During Level Flight at Transitional Flight Speeds

Oct 1962

44 NASA TN D-1481 Aerodynamic Characteristics of Four-Duct Tandem VTOL-Aircraft Configurations

Jan 1963

45 NASA TN D-1509 Propeller Slipstream Effects as Determined from Wing Pressure Distribution on a Large-Scale VTOL Model at Static Thrust

Dec 1962

46 NASA TN D-1517 Hovering Characteristics of a Rotor Having an Airfoil Section Designed for a Utility Type of Helicopter

Dec 1962

47 NASA TN D-1650 Aerodynamic Characteristics of a Large-Scale Model with Two High Disk-Loading Fans Mounted in the Wing

Jan 17 1963

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48 NASA TN D-1766 Wind-Tunnel Tests of Two VTOL Propellers in Descent

c.a.1963

49 NASA TN D-1857 Large-Scale Wind-Tunnel Tests of Descent Performance of an Airplane Model with a Tilt Wing and Differential Propeller Thrust

Oct 1964

50 NASA TN D-2014 Wing Pressure Measurements within the Propeller Slipstream for a Large-Scale V/STOL Wind-Tunnel Model Simulating Transition

Oct 1963

51 NASA TN D-2231 A Flight Investigation of the Performance, Handling Qualities, and Operational Characteristics of a Deflected Slipstream STOL Transport Airplane Having Four Interconnected Propellers

Mar 1964

52 NASA TN D-2254 Transition Characteristics of a VTOL Aircraft Powered by Four Ducted Tandem Propellers

Apr 1964

53 NASA TN D-2477 Effects of Gross Changes in Static Directional Stability on V/STOL Handling Characteristics Based on a Flight Investigation

Oct 1964

54 NASA TN D-2538 Wind-Tunnel Investigation of a Tilt-Wing VTOL Airplane with Articulated Rotors

Mar 1965

55 NASA TN D-2788 A Visual Flight Investigation of Hovering and Low-Speed VTOL Control Requirements

Apr 1965

56 NASA TN D-3936 Comparison of Flight-Measured Helicopter Rotor-Blade Chordwise Pressure Distributions with Static Two-Dimensional Airfoil Characteristics

May 1967

57 NASA TN D-4062 Full-Scale Investigation of the Aerodynamic Characteristics of a Model Employing a Sailwing Concept

Jul 1967

58 NACA TN 492 The Aerodynamic Analysis of the Gyroplane Rotating-Wing System

Mar 1934

59 NACA TN 1192 Charts Showing Relations Among Primary Aerodynamic Variables for Helicopter-Performance Estimation

Feb 1947

60 NACA TN 1250 Effect of Blade Stalling on the Efficiency of a Helicopter Rotor as Measured in Flight

Apr 1947

61 NACA TN 1289 Full-Scale Investigation of the Aerodynamic Characteristics of a Typical Single-Rotor Helicopter in Forward Flight

May 1947

62 NACA TN 1430 A Theoretical Study of the Dynamic Properties of Helicopter-Blade Systems

Nov 1948

63 NACA TN 1666 Flight Investigation of Effects of Rotor-Blade Twist on Helicopter Performance in the High-Speed and Vertical-Autorotative-Descent Conditions

Aug 1948

64 NACA TN 1698 Effect of Wind Velocity on Performance of Helicopter Rotors as Investigated with the Langley Helicopter Apparatus

Oct 1948

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65 NACA TN 1906 An Analytical Study of the Steady Vertical Descent in Autorotation of Single-Rotor Helicopters

Jun 1949

66 NACA TN 1983 Longitudinal Flying Qualities of Several Single-Rotor Helicopters in Forward Flight

Nov 1949

67 NACA TN 2226 Theoretical Analysis of Oscillations in Hovering of Helicopter Blades with Inclined and Offset Flapping and Lagging Hinge Axes

Dec 1950

68 NACA TN 2277 Effects of Compressibility on the Performance of Two Full-Scale helicopter Rotors

Jan 1951

69 NACA TN 2474 Empirical Relation Between Velocity, Thrust, and Rate of Descent of a Helicopter Rotor as Determined by Wind-Tunnel Tests on Four Model Rotors

Oct 1951

70 NACA TN 2656 A Blade-Element Analysis for Lifting Rotors That is Applicable for Large Inflow and Blade Angles and Any Reasonable Blade Geometry

Jul 1952

71 NACA TN 2665 An Extension of Lifting Rotor Theory to Cover Operation at Large Angles of Attack and High Inflow Conditions

Apr 1952

72 NACA TN 2847 Section Characteristics of a 10.5-Percent-Thick Airfoil with Area Suction as Affected by Chordwise Distribution of Permeability

Dec 1952

73 NACA TN 2943 The Attenuation Characteristics of Four Specially Designed Mufflers Tested on a Practical Engine Setup

May 1953

74 NACA TN 3022 Method for Studying Helicopter Longitudinal Maneuver Stability

Oct 1953

75 NACA TN 3182 Manual of the ICAO Standard Atmosphere Calculations by the NACA

May 1954

76 NACA TN 3237 Hovering Performance of a Helicopter Rotor Using NACA 8-H-12 Airfoil Sections

Aug 1954

77 NACA TN 3238 Review of Information on Induced Flow of a Lifting Rotor

Aug 1954

78 NACA TN 3241 Airfoil Section Characteristics at High Angles of Attack

Aug 1954

79 NACA TN 3242 Preliminary Results from Flow-Field Measurements Around Single and Tandem Rotors in the Langley Full-Scale Tunnel

Nov 1954

80 NACA TN 3304 Investigation of the Aerodynamic Characteristics of a Model Wing-Propeller Combination and of the Wing and Propeller Separately at Angles of Attack up to 90 degrees

Nov 1954

81 NACA TN 3354 Gust Experience of a Helicopter and an Airplane in Formation Flight

Dec 1954

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82 NACA TN 3361 Aerodynamic Characteristics of NACA 0012 Airfoil Section at Angles of Attack from 0 to 90 Degrees

Jan 1955

83 NACA TN 3366 A Method for Studying the Transient Blade-Flapping Behavior of Lifting Rotors at Extreme Operation Conditions

Jan 1955

84 NACA TN 3440 Hovering Flight Tests of a Four-Engine-Transport Vertical Take-off Airplane Model Utilizing a Large Flap and Extensible Vanes for Redirecting the Propeller Slipstream

May 1955

85 NACA TN 3616 Charts for Estimating Rotor-Blade Flapping Motion of High-Performance Helicopters

Mar 1956

86 NACA TN 3625 Investigation of the Propulsive Characteristics of a Helicopter-Type Pulse-Jet Over a Range of Mach Numbers and Angles of Yaw

Jan 1956

87 NACA TN 3630 Hovering-Flight Tests of a Model of a Transport Vertical-Take-Off Airplane with Tilting Wings and Propellers

Mar 1956

88 NACA TN 3745 Transition-Flight Tests of a Model of a Low-Wing Transport Vertical-Take-Off Airplane with Tilting Wing and Propellers

Sep 1956

89 NACA TN 3850 Experimental Investigation on the Langley Helicopter Test Tower of Compressibility Effects on a Rotor Having NACA 63sub2-015 Airfoil Sections

Dec 1956

90 NACA TN 3855 The Effect of Forward-Flight Speed on the Propulsive Characteristics of a Pulse-Jet Engine Mounted on a Helicopter Rotor

Jan 1957

91 NACA TN 3690 Normal Component of Induced Velocity in the Vicinity of a Lifting Rotor with a Nonuniform Disk Loading

Apr 1956

92 NACA Technical Note TN 3691 Analysis and Comparison with Theory of Flow-Field Measurements Near a Lifting Rotor in The Langley Full-Scale Tunnel

Apr 1956

93 NACA TN 3921 Approximate Solution for Streamlines About a Lifting Rotor Having Uniform Loading and Operating in Hovering or Low-Speed Vertical Flight Conditions

Feb 1957

94 NACA TN 4124 Effect of Ground Proximity on the Aerodynamic Characteristics of a Four-Engine Vertical-Take-Off-And-Landing Transport-Airplane Model with Tilting Wing and Propellers

Sep 17 1957

95 NACA TN 4131 Transition-Flight Investigation of a Four­Engine-Transport Vertical-Take-Off Airplane Model Utilizing a Large Flap and Extensible Vanes for Redirecting the Propeller Slipstream

Dec 1957

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96 NACA TN 4239 Experimental Investigation of the Drag of Flat Plates and Cylinders in the Slipstream of a Hovering Rotor

Apr 1958

97 NACA TN 4356 Effects of Compressibility on Rotor Hovering Performance and Synthesized Blade-Section Characteristics Derived from Measured Rotor Performance of Blades Having NACA 0015 Airfoil Tip Sections

Sep 1958

98 NACA TN 4357 Lift and Profile-Drag Characteristics of an NACA 0012 Airfoil Section as Derived from Measured Helicopter-Rotor Hovering Performance

Sep 1958

3 1 Air Ministry Aeronautical Research Committee – Reports and Memoranda No. 1132. On the Vertical Ascent of a Helicopter by H. Glauert, M.A.

Nov 1927

2 NACA TM No. 367 Application of the “Magnus Effect” to the Wind Propulsion of Ships

Nov 17 1924

3 Induced Flow Near a Rotor and Its Application to Helicopter Problems by Harry H. Heyson

Apr 16-20 1958

4 NASA TM X-680 Wind-Tunnel Investigation of the Aerodynamic and Structural-Deflection Characteristics of an Inflatable Airplane

Aug 1962

5 NASA TR R-14 A Method for Calculation of Hydrodynamic Lift for Submerged and Planning Rectangular Lifting Surfaces

1959

6 NASA TR R-124 Linearized Theory of Wind-Tunnel Jet-Boundary Corrections and ground Effect for VTOL-STOL Aircraft

1962

NACA ANNUAL REPORTS 4 1 National Advisory Committee on Aeronautics (NACA)

Twentieth Annual Report Numbers 475-507 1934

2 National Advisory Committee on Aeronautics (NACA) Twenty-Fourth Annual Report Numbers 612-644

1938

3 National Advisory Committee on Aeronautics (NACA) Twenty-Fifth Annual Report Numbers 645-680

1939

4 National Advisory Committee on Aeronautics (NACA) Twenty-Sixth Annual Report Numbers 681-703

1940

5 National Advisory Committee on Aeronautics (NACA) Twenty-Seventh Annual Report Numbers 704-726

1941

6 Large Photo of Convair XFY-1 Undated 7 Miscellaneous Helicopter Photos and Negatives Undated

5 1 Proceedings of V/STOL Technology and Planning Conference AFFDL

Sep 23-25 1969

2 Photos of Helicopters and 1962 Redesignation Letter Various

13

3 Vertical Take Off and Landing Concepts Applicable to Drones/RPVs(U) Appendix G-11

1974

4 Helicopter Photos Various 5 Folder of NACA Reports – Reports No. 352, 460, 537,

586, 628, 664, 586, 573, 574, 648, 651, 678, 627, 665, 575, 540, 642, 680, 592, 662, 652, 546.

1933-1939

NACA REPORTS - BOUNDARY LAYER CONTROL, JET CIRCULATION

6 1 Report No. 77-0076 Circulation Control – An Updated Bibliography of DTNSRDC Research and Selected Outside References

Sep 1977

2 Research on Elliptical Airfoil with Jet Circulation Control Contract# N00014-67-A0126 Univ. of Texas

Jan 1969

3 Proposal No. 148 Theoretical and Experimental Analysis of the Jet Circulation Control Airfoil Nielsen Engineering & Research, Inc.

Mar 7 1968

4 The Laminar Flow Control Presentation for the Aeronautical Systems Division Northrop

May 3-4 1962

5 Boundary Layer Control by Porous Suction by H.G. Lew & R.D. Matieu Penn. State Univ. Contract# AF18(600)­575

Jun 1954

6 Report No. 071 Suction and Blowing Tests on the Cessna 309 Mock-Up by Friedrich Wagner Univ. of Wichita

Apr 1952

7 Research Report No. 15 A Simplified Procedure for Calculating Boundary Later Control Systems for Unflapped Airfoils by J.J. Cornish, III Miss. State Univ.

Feb 28 1958

8 Research Report No. 19 Practical High Lift Systems Using Distributed Boundary Layer Control by J.J. Cornish, III Miss. State Univ.

Dec 10 1958

9 TR No. 8 Simplicity with Accuracy in the Computation of Spanwise Lift Distribution Stout Skycraft Corp.

Jan 20 1941

10 A.R.C. TR C.P. No. 82 Power Requirements for Distributed Suction for Increasing Maximum Lift UK Ministry of Supply

1952

11 WADC TR 52-196 Design of Boundary-Layer-Control Suction and Blowing Ducts with Arbitrary Flow Distributions

Sep 1952

12 AGARD-CP-126 Military Applications of V/STOL Aircraft Volume 1

Oct 23-25 1972

13 AHS 30th Annual Forum – Paper 823 U.S. Navy VTOL Automatic Landing System Development Program by Robert S. Buffum, Richard W. Huff & Capt. Gerard L. Keyser Flight Test Div., Pax River

May 1974

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14 Document No. 12055-FR1 Experimental Investigations of Flight Control Surfaces Using Modified Air Jets Contract# N00019-67-C-0260 Honeywell

Nov 1969

15 Background, Recent Developments and Objectives in V/STOL Aircraft Fairchild

C.A. 1965

16 NASA Memo 2-27-59A Low-Speed Tests of Semispan-Wing Models at Angles of Attack from 0o to 180o

Mar 1959

17 NASA TN D-316 Study of the Aerodynamic Forces and Moments on Bodies of Revolution in Combined Pitching and Yawing Motions

Apr 1960

18 NASA TN D-660 Effects of Various Arrangements of Slotted and Round Jet Exits on the Lift and Pitching-Moment Characteristics of a Rectangular-Base Model at Zero Forward Speed

Feb 1961

19 NASA TN D-720 Effect of Ratio of Jet Area to Total Area and of Pressure Ratio on Lift Augmentation of Annular Jets in Ground Effect under Static Conditions

Mar 1961

20 NASA TN D-727 Ground Interference Effects Apr 1961 21 NASA TN D-786 Investigation of the Longitudinal

Characteristics of a Large-Scale Jet Transport Model Equipped with Controllable Thrust Reversers

Mar 1961

22 NASA TN D-789 Aerodynamics of a Fan-In-Fuselage Model

May 1961

23 NASA TN D-818 Method of Calculating Induced Velocities at the Blades of a Slightly Inclined Propeller with Constant Circulation

May 1961

24 NASA TN D-969 Effect of Groundboard height on the Aerodynamic Characteristics of a Lifting Circular Cylinder Using Tangential Blowing from Surface Slots

Oct 1961

25 NACA TN No. 323 Wind Tunnel Tests on Airfoil Boundary Later Control Using a Backward Opening Slot

Oct 1929

26 NACA TN No.340 Full Scale Drag Tests on Various Parts of Fairchild (FC-2W2) Cabin Monoplane

May 1930

27 NACA TN No.507 The Effects of Equal-Pressure Fixed Slots on the Characteristics of a Clark Y Airfoil

Oct 1934

28 NACA TN No.624 Performance Characteristics of Venturi Tubes Used in Aircraft for Operating Air-driven Gyroscopic Instruments

Nov 1937

29 NACA TN No.640 Interference of Wing and Fuselage from Tests of 18 Combinations in the NACA Variable-Density Tunnel - Combinations with Split Flaps

Mar 1938

30 NACA TN No.641 Interference of Wing and Fuselage from Tests of 17 Combinations in the NACA Variable-Density Tunnel – Combinations with Special Junctions

Mar 1938

15

31 NACA TN No.642 Interference of Wing and Fuselage from Tests of Eight Combinations in the NACA Variable-Density Tunnel – Combinations with Tapered Fillets and Straight-Side Junctions

Mar 1938

32 NACA TN No.691 Some Elementary Principles of Shell Stress Analysis with Notes on the Use of the Shear Center

Mar 1939

33 NACA TN No.692 Some Fundamental Considerations in Regard to the Use of Power in Landing an Airplane

Mar 1939

34 NACA TN No.695 The Effects of Some Common Surface Irregularities on Wing Drag

Mar 1939

35 NACA TN No.699 Tests of NACA 23012 Airfoil with Slotted Deflector Flap

Apr 1939

36 NACA TN No.702 Wind-Tunnel Tests of Several Forms of Fixed Wing Slot in Combination with a Slotted Flap on an NACA 23012 Airfoil

Apr 1939

37 NACA TN No.705 Wind-Tunnel Investigation of Ground Effect on Wings with Flaps

May 1939

38 NACA TN No.714 Flight Tests of Retractable Ailerons on a Highly Tapered Wing

Jun 1939

39 NACA TN No.715 Wind-Tunnel Investigation of an NACA 23012 Airfoil with Two Arrangements of a Wide-Chord Slotted Flap

Jun 1939

40 NACA TN No.719 The Effects of Partial-Span Slotted Flaps on the Aerodynamic Characteristics of a Rectangular and a Tapered NACA 23012 Wing

Jul 1939

41 NACA TN No.728 Wind-Tunnel Investigation of an NACA 23012 Airfoil with Two Arrangements of a 40­Precent-Chord Slotted Flap

Sep 1939

42 NACA TN No.732 A Simplified Method of Obtaining Span Load Distributions

Oct 1939

43 NACA TN No.837 Notes on the Stability and Control of Tailless Airplanes

Dec 1941

44 NACA Technical Note 2502 Examples of Three Representative Types of Airfoil-Section Stall at Low Speed

Sep 1951

45 NACA Technical Note 2659 A Miniature Electrical Pressure Gage Utilizing a Stretched Flat Diaphragm

Apr 1952

46 NACA Technical Note 3918 Wind-Tunnel Investigation of Effect of Propeller Slipstreams on Aerodynamic Characteristics of a Wing Equipped with a 50-Percent-Chord Sliding Flap and a 30-Percent-Chord Slotted Flap

Feb 1957

47 NACA TM No. 475 Recent researches on the Air Resistance of Spheres

Aug 1928

48 NACA TM No.557 Measurement of Profile Drag on an Airplane in Flight by the Momentum Method Part I

Mar 1930

16

49 NACA TM No.558 Measurement of Profile Drag on an Airplane in Flight by the Momentum Method Pt. II

Mar 1930

50 NACA TM No.545 The Balance of Moments and the Static Longitudinal Stability of Airplanes

Dec 1929

51 NACA TM No. 563 Balanced and Servo Control Surfaces May 1930 52 NACA TM No. 567 The Magnus Effect in Theory and in

Reality May 1930

53 NACA TM No. 612 Static Longitudinal Stability of “ENTE” Airplanes

Mar 1931

54 NACA TM No. 794 Chief Characteristics and Advantages of Tailless Airplanes

May 1936

55 NACA TM No. 850 Engines and Propellers for Powered Gliders and Light Airplanes

Mar 1938

56 NACA TM No. 867 Theoretical Study of Various Airplane Motions After Initial Disturbance

Jun 1938

57 NACA TM No. 900 The Effect of the Masses of the Controls on the Longitudinal Stability with Free Elevator

Jul 1939

58 NACA TM No. 906 Forces and Moments on a Yawed Airfoil

Aug 1939

59 NACA TM No. 974 Boundary Layer Removal by Suction Apr 1941 60 NACA TM No. 990 Contribution to the Aerodynamics of

Rotating-Wing Aircraft Part II 1941

61 NACA TM No. 1011 Pressure Distribution on Wings in Reversed Flow

Apr 1942

62 NACA Report No. 315 Aerodynamic Characteristics of Airfoils – VI

1929

63 NACA Report No. 331 Collection of Wind-Tunnel Data on Commonly Used Wing Sections

1929

64 NACA Report No. 400 The Aerodynamic Characteristics of a Slotted Clark Y Wing as Affected by the Auxiliary Airfoil Position

1931

65 NACA Report No. 411 Theory of Wing Sections of Arbitrary Shape

1931

66 NACA Report No. 419 Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack –I-Ordinary Ailerons on Rectangular Wings

1932

67 NACA Report No. 422 Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack –II- Slotted Ailerons and Frise Ailerons

1932

68 NACA Report No. 423 Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack – III-Ordinary Ailerons Rigged Up 10o When Neutral

1932

69 NACA Report No. 424 Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack – IV-Floating Tip Ailerons on Rectangular Wings

1932

17

70 NACA Report No. 437 The Effect of Area and Aspect Ratio on the Yawing Moments of Rudders at Large Angles of Pitch on Three Fuselages

1932

71 NACA Report No. 439 Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack –V-Spoilers and Ailerons on Rectangular Wings

1932

72 NACA Report No. 444 Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack –VI-Skewed Ailerons on Rectangular Wings

1932

73 NACA Report No. 450 The Calculation of Take-Off Run 1932 74 NACA Report No. 494 A Flight Investigation of the

Lateral Control Characteristics of Short Wide Ailerons and Various Spoilers with Different Amounts of Wing Dihedral

1934

75 NACA Report No. 496 General Theory of Aerodynamic Instability and the Mechanism of Flutter

1935

76 NACA Report No. 499 Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack –XII-Upper-Surface Ailerons on Wings with Split Flaps

1934

77 NACA Report No. 517 Flight Investigation of Lateral Control Devices for Use with Full-Span Flaps

1935

78 NACA Report No. 518 The Drag of Airplane Wheels, Wheel fairings and Landing Gears – II Nonretractable and Partly Retractable Gears

1935

79 NACA Report No. 530 Characteristics of the NACA 23012 Airfoil from Tests in the Full-Scale and Variable-Density Tunnels

1935

80 NACA Report No. 541 Aerodynamic Characteristics of Wings with Cambered External-Airfoil Flaps, Including Lateral Control with a Full-Span Flap

1935

81 NACA Report No. 552 Wind-Tunnel Tests of 10-Foot-Diameter Autogiro Rotors

1936

82 NACA Report No. 554 Wind-Tunnel Investigation of Ordinary and Split Flaps on Airfoils of Different Profile

1936

83 NACA Report No. 573 Aerodynamic Characteristics of NACA 23012 and 23021 Airfoils with 20-Percent-Chord External-Airfoil Flaps of NACA 23012 Section

1936

84 NACA Report No. 579 A Study of the Two-Control Operation of an Airplane

1936

85 NACA Report No. 586 Airfoil Section Characteristics as Affected by Variations of the Reynolds Number

1937

86 NACA Report No. 602 Wind-Tunnel and Flight Tests of Slot-Lip Ailerons

1937

87 NACA Report No. 605 Resume and Analysis of NACA Lateral Control Research

1937

18

88 NACA Report No. 654 General Airplane Performance 1939 89 NACA Report No. 669 Airfoil Section Data Obtained in

the NACA Variable-Density Tunnel as Affected by Support Interference and Other Corrections

1939

90 NACA Report No. 677 Wind-Tunnel Investigation of an NACA 23021 Airfoil with Various Arrangements of Slotted Flaps

1939

91 NACA Report No. 679 Wind-Tunnel Investigation of an NACA 23012 Airfoil with a Slotted Flap and Three Types of Auxiliary Flap

1939

92 NACA Report No. 716 A Simplified Theoretical Method of Determining the Characteristics of a Lifting Rotor in Forward Flight

1941

93 NACA Wartime Report CB 3E27 Characteristics of an NACA 66,S-209 Section Hydrofoil at Several Depths

May 1943

94 NACA Wartime Report L4C28 Preliminary Tank Experiments with a Hydrofoil on a Planing-Tail Seaplane Hull

Mar 1944

95 NACA Wartime Report L5A13a Wind-Tunnel Tests of a Dual-Rotating Propeller Having One Component Locked or Windmilling

Jan 1945

96 NACA Wartime Report L4C24 On the Flow of a Compressible Fluid by the Hydrograph Methods – I-Unification and Extension of Present-Day Results

Mar 1944

97 NACA Wartime Report L4D06 Preliminary Tank Tests of an Outboard Float Having the Form of a Streamline Body of Revolution Fitted with a Hydrofoil

Apr 1944

98 NACA TN No. 1683 An Experimental Investigation of an NACA 631-012 Airfoil Section with Leading Edge Suction Slots

Aug 1948

99 NACA TN No. 1741 Exploratory Wind-Tunnel Investigation of the Effectiveness of Area Suction in Eliminating Leading-Edge separation over an NACA 641A212 Airfoil

Nov 1948

Series III: AVRO Avrocar, 1958-1990

Box File Description Date

7 1 AVRO/SPG/TR 125 Issue 6 Airplane Weight Moment of Inertia and C. of G. Status – AVROCAR-

Feb 1959

2 AVRO/SPG/TR267 Test Data Report for The Full Scale 20o Wingtip Segment of the AVROCAR Contract# AF33(600) 37496 AVRO

May 1959

19

3 AVRO/SPG/TR 265 Part 2 & 3 Test Data Report for 1/5 Scale AVROCAR Model, Forward Flight Characteristics Contract# AF 33(600)-30161 AVRO

Dec 1959

4 AVRO/SPG/TR183 Mass Flow and Thrust Calibration of Transonic Sting Model Contract# AF33(600)30161 AVRO

Jul 1958

5 AVRO/SPG/TR264 Force Data Results and Analysis of a Second Series of Tests on a 1/6 Scale Model AVRO

Apr 1959

6 AVRO/SPG/TR 275 System 606A VTOL Fighter-Bomber Project Load and Stress Survey Turborotor Contract# Af33(600)-30161 AVRO

Jan 1959

7 AVRO/SPG/TR264 Appendix Force Data Results and Analysis of a Second Series of Tests on a 1/6 Scale Model AVRO

Apr 1959

8 AVRO 500/AREO TEST/408 Avrocar Continuation Test Program Report on Phase 2 Tests of an Avrocar in the 40x80 Foot Wind Tunnel at NASA Ames research Center Vol. 1Contract# AF33(600)-42163 AVRO

May 1961

9 AVRO/SPG/TR 276 System 606A VTOL Fighter-Bomber Project: Notes on the Preliminary Performance Calculations Contract AF33(600)-30161 AVRO

Jan 1961

10 AVRO 600 (PROJ) 2 Preliminary Trade-Off Study Contract# AF33(600)-39722 AVRO

Jan 1960

11 AVRO/SPG/TR 310 Further Tests on J69 Exhaust Ducting for AVROCAR Contract# AF33(600)-37496 AVRO

Jan 1960

12 AVRO 500/AERO TEST/410 Avrocar Continuation Program Data Report for 1/20 Scale Avrocar Model Contract# AF33(600)-42163 AVRO

Jan 1961

13 AVRO/SPG/TR 187 Report on Avrocar Analog Computing Program Phase 1 and Phase 2 Contract# AF33(600)30161 Supplementary Agreement No. 5 AVRO

Nov 1958

14 AVRO Progress Report No. 6 AVROCAR 1: US Army Designation VZ-9A V Contract# AF33(600)37496 AVRO

Feb. - Mar 1959

15 AVRO 500/PERF/411 Summary Review of the Continuation Test Program for the Avrocar: Including Review of Allied Programs Contract# AF33(600)-42163 AVRO

May 1961

16 AVRO/SPG/TR 205 ISSUE 1 Strength Summary and Operating Restrictions Contract# AF33(600)-37496 AVRO

Apr 1959

17 AVRO/SPG/TR 304 Tethered and Free Flight Tests of the AVROCAR Fitted with Nozzle Spoiler Controls Contract# AF33(600)-37496 AVRO

Dec 1959

18 Evolution of an Engineering Miracle; Flight Dynamics Laboratory Article

Oct 1988

19 AVRO P450/PERF/1 Mobile Ground Effect Machine Preliminary Report AVRO

Jun 1960

20

20 AVRO/SPG/TR 308 Data Report for the 1/20 Scale Avrocar Model Focusing Ring Control Static Tests Contract# AF33(600)-37496 Supplementary Agreement No. 1 AVRO

Undated

21 AVRO/SPG/TR 254 The Avrocar Design Contract# AF33(600) 30161 AVRO

Jan 1959

22 The AVRO VZ-9 Experimental Aircraft (AVROCAR) Lessons Learned AVRO

Sep 17-19,1990

23 AVRO P470/THEORETICAL AERO/3 The Two Dimensional Airfoil in Incompressible Flow with Arbitrary Mass Flow Through a Central Gap AVRO

Jun 1960

24 AVRO/SPG/TR265 Part 1 Data Report for the 1/5 Scale Avrocar Model Tests Contract# AF33(600)-30161 AVRO

Nov 1959

25 AVRO/SPG/TR 263 The Effect of the Incorrect Assumptions on Avrocar Static Thrust and Turborotor Running Conditions Contract# AF33(600)37496 Supplementary Agreement No. 5 AVRO

Nov 1958

26 Avrocar Turborotor Test Specifications Contract# AF33(600)-37496 Supplemental Agreement Proposal AVRO

Jan 22 1959

27 AVRO/SPG/TR264 Force Data Results and Analysis of a Second Series of Tests on a 1/6 Scale Model AVRO

Apr 1959

8 1 AVRO Review of AVRO G.E.T.O.L/V.T.O.L Future Development

Dec 8-9 1959

2 AVRO/SPG/TR 205 Issue 1 Strength Summary and Operating Restrictions AVROCAR 1 Contract# AF33(600)-37496 AVRO

Apr 1959

3 AVRO/SPG/TR 308 Data Report for the 1/20 Scale AVROCAR model Focusing Ring Control Static Tests Contract# AF33(600)-37496 Supplemental Agreement No. 1 AVRO

Undated

4 Model Specification AVRO Aircraft Project AVROCAR 1 US Army Designation VZ-9AV

May 20 1958

5 AVRO/SPG/TR 254 The AVROCAR Design Contract# AF33(600)-30161

Jan 1959

6 AVRO/SPG/TR 249 Report on AVROCAR Analog Computing Program Phase 3 Contract# AF33(600)-30161 Supplementary Agreement No. 5 AVRO

Feb 1959

7 Progress Report No. 3 AVROCAR 1 US Army Designation VZ-9AV Contract# AF33(600)-37496

Aug 1 1958 –Sep 30 1958

8 AVRO/SPG/TR 197 ADDENDUM No. 1 Specification for Tests of an AVROCAR in the 40 Foot X 80 Foot Wind Tunnel at NASA Ames Aeronautical Laboratories Contract# AF33(600)-37496 Supplemental Agreement No. 1 AVRO

Feb 1960

21

9 AVRO System 606A Bi-Monthly Progress Report No. 11 1 November 1958 -31 December 1958 Contract# AF33(600)30161 Supplemental Agreement No. 5 AVRO

Jan 20 1959

10 AVRO Program Planning Report Pre-Phase 1 Part 1 and Part 2 – Development Program VTOL Supersonic Aircraft AVRO

Sep 30 1959

11 AVRO/SPG/TR 280 Test Specification for the Research Flight Test Program AVROCAR 1 AVRO

Undated

12 500/AERO TEST/405 AVROCAR Continuation Test Program Specification for the Phase 2 Tests of an AVROCAR in the 40x80 Foot Wind Tunnel at NASA Ames Research Center Contract# AF33(600)-42163 (S.W.8) AVRO

Dec 1960

13 AVRO/SPG/TR 312 Note on the AVROCAR Simulator for Hovering and Low Speed Flight AVRO

Feb 1960

14 Report CR-300 Summary TR AVROCAR Turborotor Development Program I.D. No. 60 RDZ-2227

Feb 1960

15 AVRO/SPG/TR 195 AVROCAR Ground and Flight Test Specifications AVRO

Nov 1958

16 500/S&C/428 Canadian Government Program for the AVROCAR Phase 1 Stability and Control Contract# T.B.570345 and Serial No. 9-BX-0-8 (S.O.W. Para 2.1.4)

May 1961

17 500/AERO TEST/415 Issue 2 AVROCAR Continuation Test Program Instrumentation Specification For AMES Tunnel Tests 1st AVROCAR Vehicle Contract# AF33(600)-42163 (S.W.5) AVRO

Dec 1960

18 Progress Report No. 10 AVROCAR 1 US Army Designation VZ-9AV Contract# AF33(600)-37496 and Supplemental Agreement No. 1 AVRO

Oct - Nov 1959

19 500/PROJ/6 Progress Report No. 3 AVROCAR 1 US Army designation VZ-9AV Contract# AF33(600)-42163 (S.W. 11) AVRO

Nov 1960

20 AVROCAR 1 US Army Designation VZ-9A V Cumulative Cost Report Supplement to AVROCAR Progress Report No. 5Contract# AF33(600)37496 AVRO

Feb 28 1959

21 Progress Report No. 11 AVROCAR 1 US Army Designation VZ-9AV Contract# AF33(600)-37496 and Supplemental Agreement No. 1 AVRO

Dec 1959 - Jan 1960

22 AVRO/SPG/TR 304 Tethered and Free Flight Tests of the AVROCAR Fitted with Nozzle Spoiler Controls Contract# AF33(600)-37496 Supplemental Agreement No. 1 AVRO

Dec 1959

23 500/PROJ/1 Progress Report No. 1 Canadian Government Program for the AVROCAR AVRO

Jul 31 1960

22

24 500/PERF/430 Canadian Government Program for the AVROCAR Phase 1 – Comparison of the Direct Operating Costs of the Light Aircraft with Developed Versions of the AVROCAR Contract# TB570345 Serial No. 9-BX-0-8 (S.O.W. Para 2.1.5) AVRO

Apr 1961

25 AVRO/SPG/TR 300 Revision of Propulsion Estimates AVROCAR 1 Contract# AF33(600)-37496 AVRO

Dec 1959

26 AVRO Program Planning Report AVROCAR 1 US Army Designation VZ-9AV

May 1 1958

27 AVRO/SPG/TR 305 Tests of the AVROCAR in the Static Rig Contract# Af33(600)-37496 Supplemental Agreement No. 1 AVRO

Dec 1959

28 Review of AVROCAR Development Prospects Apr 6-7 1960 29 AVRO/SPG/TR 174 A Brief Technical Description of the

AVROCAR Contract# AF33(600)30161 Supplementary Agreement No. 3 AVRO

May 1958

30 Progress Report No. 5 AVROCAR 1 – US Army Designation VZ-9AV Contract# AF33(600)37496 AVRO

Dec 1 1958 –Jan 31 1959

31 Progress Report No. 1 AVROCAR 1 – US Army Designation VZ-9AV Contract# AF33(600)37496 AVRO

Feb 1 – Jun 30 1958

32 500/PERF/427 Canadian Government Program for the AVROCAR Phase 1 – Performance- Contract# TB570345 Serial No. 9-BX-0-8 (S.O.W. Para 2.1.5)

Mar 1961

9 1 AVRO/SPG/TR 242 Tests on J69 Intake and Exhaust Ducting For AVROCAR Contract# AF33(600)-37496 Supp. Agree. #1 AVRO

Apr 1959

2 AVRO/SPG/TR 264 Appendix – Force data Results and Analysis of a Second Series of Tests on a 1/6 Scale Model AVRO

Apr 1959

3 AVRO/SPG/TR 265 Part 2 & 3 1/5 Scale AVROCAR Model Forward Flight Characteristics Contract# AF33(600)-30161 Supp. Agree. #5 AVRO

Dec 1959

4 AVRO/SPG/TR 266 Data Report for the 1/20 Scale AVROCAR Model Tests Contract# AF33(600)-37496 AVRO

Jun 1959

5 AVRO/SPG/TR 300 Revision of Propulsion Estimates AVROCAR 1 Contract# AF33(600)-37496 AVRO

Dec 1959

6 AVRO/SPG/TR 308 Data Report for the 1/20 Scale AVROCAR Model Focusing Ring Control Static Tests Contract# AF33(600)-37496 Supp. Agree. #1 AVRO

C.A. 1960

7 AVRO/SPG/TR 408 AVROCAR Continuation Test Program Report on Phase 2 Tests of an AVROCAR in the 40x80 Foot Wind Tunnel at NASA Ames Research Center Contract# AF33(600)-42163 (S.W. 9) AVRO

May 1961

23

8 NASA TN D-1432 Large-Scale Wind-Tunnel Tests of a Circular Plan-Form Aircraft with a Peripheral Jet for Lift, Thrust, and Control AVRO

Feb 1963

9 The AVRO VZ-9 Experiment Aircraft – Lessons Learned by Daniel C. Murray Wright Research & Development Center – Original Manuscript Plus Copies

C.A. 1962

10 AVROCAR Photos C.A. 1960 11 Comparative Paper of AVROCAR 1, ADAM III, Short

SC-1, Dassault Mirage IIIV, Entwicklungsring Sud EWR VJ 101C, Verinigte Flugtechnische werke VAK-191B, US/FRG V/STOL Tactical Fighter and Dornier 31. (partial package)

C.A. 1972

12 The AVRO VZ-9 Experiment Aircraft – Lessons Learned by Daniel C. Murray Wright Research & Development Center – Slide Presentation Associated with #9 above (20 slides)

C.A. 1962

13 Progress Report No. 2 – AVROCAR 1 (Army VZ-9AV) Jul 1 1958 to Jul 31 1958 Contract# AF33(600)-37496

Aug 30 1958

14 Progress Report No. 6 – AVROCAR 1 (Army VZ-9AV) Feb and Mar 1959 Contract# AF33(600)-37496

C.A. Apr 1959

15 Progress Report No. 9 – AVROCAR 1 (Army VZ-9AV) Aug and Sep 1959 Contract# AF33(600)-37496 and Supp. Agree. #1

C.A. Oct 1959

16 System 606A Bi-Monthly Progress Report No. 17 Contract# AF33(600)-30601 and Supp. Agree. #3,5,6.

C.A. Jan 1960

17 Proposal for AVROCAR No. 2 C.A. 1960 18 Proposal for AVROCAR No. 3 C.A. 1960 19 AVROCAR Documents (3) 1959-1960 20 Report No. AVRO/SPG/TR157 Frequency Response Tests

of a Pneumatic Control System – System 606A- Contract# AF33(600)30161 AVRO

May 1958

21 Report No. AVRO/SPG/TR296 Results of Frequency Response Tests of the Pilot Control Bellows for the AVROCAR Contract AF33(60)-30161 AVRO

Jan 1960

22 Report No. AVRO/SPG/TR311 Static Rig and Flight Tests of the AVROCAR Fitted with the Focusing Ring Control Contract# AF33(600)-37496 Supp. Agreement No. 1 AVRO

Feb 1960

23 Report No. 600/PERF/17 Vertical Take-Off & Landing Performance Using an Ejector Lift Augmentation System Contract# AF33(600)-39722 AVRO

Jul 1960

24 Report No. 500/PERF/411 Summary Review of the Continuation Test Program for the AVROCAR Contract# AF33(600)-42163 AVRO

May 1961

25 Report No. FTC-TDR-61-56 AVROCAR Flight Evaluation AFFTC

Jan 1962

24

SERIES IV: Helicopters, 1934-1997

Box File Description Date

EARLY (PRE-1960) HELICOPTERS 10 1 Report D200-099-001 Estimated Performance for Bell

Model D-200 Gas Turbine Helicopter Sep 7 1951

2 Report D200-099-002 Proposal Summary for Bell Model D-200 Gas Turbine version of the H-13D – HTL-4 Helicopter

Oct 2 1951

3 Report D200-099-003 Comparative Payloads and Durations Provided by the Principle Helicopter Rotor Propulsion Systems

Sep 10 1951

4 Report D200-947-001 Detail Specification for Bell Model D-200 Gas Turbine Two Bladed Helicopter

Apr 7 1952

5 D200 Turbine Powered Helicopter Brochure Bell Sep 1951 6 Bell Model D-200 Blueprints 1951 7 NAVAER SD-377 Detail Specification for Model XHJD-1

Helicopter (Flight Test Article) (Twin Rotor) (Convertible) Contract# NOa(s)-3703

May 8 1944

8 Hiller Helicopter Blueprints 1947 9 BIS-21139 FT36-141 Model HRS-1 Helicopter, BuNo

127783 and Model HRS-2, BuNo 129017: Limited Tests, Report No. 2

Jun 18 1952

10 Report NV-1016 Evaluation of Wind- Tunnel Tests of a Dynamic Model of the XH-17 Helicopter Rotor Contract# AF 33(038)-8907 Hughes

Apr 5 1954

11 Report WCT 2366 Phase II Flight Tests of the Seibel YH­24SE Helicopter, USAF No. 51-5113

Oct 22 1951

12 Report AFFTC-TR-58-15 ARDC XH-40 Air Force Flight Evaluation

May 1958

13 Proposal to the US Army for the Procurement of Model 720 Vol.I Hiller

Sep 1951

14 Proposal to the US Army for the Procurement of Model 720 Vol.II Hiller

Sep 1951

15 Report 22-A-14 H21A Fairing Evaluation Contract# AF33(038)-12881 Piasecki

Nov 28 1953

16 Report 1460.16 An Analytical Approach to Directional Stability of a Synchropter Using the Energy Method Kellett

Nov 1945

17 Report SD-529-1 Detail Specification for HTK-1K Helicopter Single Engine Contract# NOas 57-619c

Feb 25 1957

18 Report No.230.34 A determination of the Blade Motion About the Horizontal Hinge for a Syncropter Type Helicopter in Hovering Flight Kellett

Mar 1945

25

19 Report No. 1430.25 A Study of the Hovering Stability of the XH-17 Kellett

Sep 1948

20 Report AFFTC-TR-57-15 KAMAN K-600-3 Limited Flight Evaluation

Aug 1957

21 Report R-167 Photographs of the KAMAM Model K-600 Local Crash Rescue Helicopter for the USAF

Dec 1 1956

22 Report AFFTC-TR-58-1 Flight Evaluation of Directional Stability and Control of KAMAM K-600 with Various Empennage Configurations and Stability Augmentation

Feb 1958

23 HOK-1 Blueprint – General Arrangement Dec 22 1952 24 Report 163-K-3 Rotor Development XA-5 Helicopter

Engineering Data Contract# AF 33(038) 6099 Sep 10 1952

25 Report AFFTC-TN-59-4 Limited Performance Evaluation of the H-43A Helicopter

Mar 1959

26 Report R-550 HH-43F Huskie KAMAN Aug 1964 rev. May 18 1967

27 Report R-165 KAMAN Model K-600 Weight and Balance Report

Dec 1 1956

28 AN-260HB-3 Handbook Structural Repair Navy Model HOK-1 Helicopter

Nov 15 1955

29 AN-01-260HBA-2 Handbook Maintenance Instructions Navy Model HOK-1 Helicopter

Jul 15 1955

30 Report SER-5005 Actual Weight Report – Last Aircraft_ Fifty-Fifth Aircraft (Government #55-4944 – S.S. #55996) Model H-19D Contract# AF33(600)-28552

Jul 9 1956

31 Report AFFTC-TR-55-26 H-21C Phase IV – Performance Evaluation

Dec 1955

32 Report MCRFT-2222 Phase II Flight Tests of the Piasecki HRP-1 Helicopter

May 4 1949

33 Report MCRFT-2265 Accelerated Service Test of the HRP-1 Helicopter

Feb 24 1950

34 Report SER-2078 Stress and Motion Survey of S-55, YH­19, HO4S-1 Rotor Head and Main Rotor Blades

Dec 15 1950

35 H-21C Blueprints Piasecki 1951 36 XR-8 Blueprints Kellett 1945 37 Report 1420.5 Proposal Specification for Three Place

Naval Helicopter Kellett Serial Number 16 and 16A Sep 1945

38 Report 1420.6 Proposal Specification for Three Place Naval Helicopter Kellett Serial Number 16B

Sep 1945

39 Report P-46 Flight Manual Performance Data Substantiation H-43B Local Crash Rescue Helicopter Contract# AF33(600)-36190 KAMAN

Feb 23 1959

40 KAMAN Model K-190 Utility Helicopter Brochure 1947 41 UH-2C Seasprite Brochure KAMAN Undated 42 BO-105 Boeing-Boelkow Helicopter Brochure Undated 43 Report 58-67 Three Place Instrument Trainer Helicopter May 1958

26

44 Report DR-212Preliminary Performance Report Model LZ-5-3 Helicopter DOMAN

Jul 27 1956

45 Do 132 Light Four-Seater Helicopter Brochure Dornier 1968 46 Report 8025-099-011 Research Study of a High

Performance Iriquois Helicopter Bell Apr 4 1961

47 Report R-414 Twin Turbine Utility Helicopter The Huskie III KAMAN

Oct 8 1962

48 Report 175-H-6 Preliminary Aerodynamic and Performance Analyses of MX-1660 Helicopter Rotor System Contract# AF33(600)-15613

Nov 1 1952

49 Report AR-117 Preliminary Aerodynamic Analysis of the Model A Quadrotor Convertiplane Convertawings

Nov 10 1952

50 Report R-164 A Proposal for the Local Crash Rescue Helicopter for the USAF KAMAN Model K-600

Dec 1 1956

51 Report 48-978-001 Performance Estimation for XR-12 Helicopter (Model 48) Bell

Dec 13 1946

11 1 AGARD Conference Proceedings No. 22 Fluid Dynamics of Rotor and Fan Supported Aircraft at Subsonic Speeds

Sep 1967

2 Report No. PB 111632 Rotary Wing Aircraft Handbooks and History Vol. 8 Mechanical Design and Description Contract# W33038 ac-21804(20695)

1954

3 Report No. F-TS-5408-RE The Power Requirements of the Ideal helicopter by G. Sissingh (from German)

Apr 1948

4 R. & M. No. 1730 The Flight of the Helicopter by H.B. Squire Air Ministry

1936

5 Report No. F-TS-1007-RE Investigation of the Influence of High Subsonic Velocities on the L/D of Rotary Wing Aircraft by G. Sissingh (from German)

Sep 1946

6 Report No. F-TS-1005-RE Theory of Oscillations of Blades in the Plane of Rotation by Dr. Kurt Hohenemser (from German)

Sep 1946

7 Aero Data Report No. 20 Wind-Tunnel Tests of Several Full-Scale Helicopter Rotor-Tip Lights at Subsonic Speeds

Apr 1954

8 Report No. 373 An Economical Technique for the Construction and Hovering Flight Evaluation of Dynamically Similar Helicopter Models Contract# Nonr­27015 Princeton Univ.

Nov 1956

9 Report No. TB-707-S-2 Helicopter Handling Qualities Investigation Phase II Analysis of Helicopter Stability and Control Problem Part B Physical Discussion of Helicopter Handling Qualities Contract# NOa(s)-12151 Cornell

Jun 1955

10 Proposal for a Variable Stability Helicopter Cornell Nov 1957 11 Report No. D4-943-001 Preliminary Performance

Estimates for Proposed Helicopter (Model D-4) Bell Jan 9 1942

12 Report No. E-65 Bell Aircraft Corp. Wind Tunnel Tests of Nov 15 1945

27

a #8-25-44 Anti-Torque Propeller Georgia Tech 13 Report No. E-68 Wind Tunnel tests of a Model 47 Anti-

Torque Propeller Georgia Tech Feb 1946

14 Report No. E-72 Bell Aircraft Corporation Wind Tunnel Tests of a No. 47 Anti-Torque Propeller Georgia Tech

Apr 1946

15 Report No. E-79 Wind Tunnel Tests of an X47-642-010-4 Straight Twist Anti-Yorque Propeller Georgia Tech

Jun 1946

16 Aero Data Report No.774 Report C-246 Wind-Tunnel Tests of a 0.10-Scale HRP-2 Helicopter Without Rotors Part I – Longitudinal and Lateral Characteristics with Original Afterbody

Aug 1949

17 Report No. 59V-10-3 Non-Uniform Rotor Blade Free and Forced Uncoupled Flap Bending Aero-Elastic Vibrations – Theory- Contract# AF 33(616)-238 Kellett

May 1953

18 Local Crash Rescue Considerations Brochure Bell Undated 19 Instrument Flight Investigation in Helicopters by Owen Q.

Niehaus Bell Undated

20 Practical Instrument Flying in the Helicopter by Joseph A. Cannon & Owen Q. Niehaus Bell

Undated

21 Report No. NAES INSTR 38-47 Development of Helicopter Attitude Indicator

Dec 1 1947

22 YH-16B Vibration Study without Enclosures Undated 23 Report No. SM-18311 Helicopter Vibration 1945 Douglas Apr 9 1954 24 Report No. W.T.T.#197 Aerodynamic Characteristics of

the 1/12 Scale Model of the XR-6 Helicopter Fuselage Contract# W534 ac-35340 Sikorsky

Oct 22 1943

25 Elementary Aerodynamics of Compound Rotorcraft Chapters II, III and IV

Undated

26 Report No. HTC-AD-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 5 Stability, Control and Flying Qualities Hughes

May 1966

27 Report No. 30-929-101 Engine & Rotor Tests in Hovering Flight Bell

Jul 23 1943 Dec 23 1944

28 Report No. GAE 52-4 ATI 162780 Effect of Disc Loading on the Payload Range Spectrum of a 60,000 Pound Helicopter AFIT

Aug 1952

29 Report No. YA-1532 Aerodynamic Performance of the M­30 Quadrotor Transport Helicopter Convertawings

Undated

30 Report No. AF TR 6272 Draft Performance Testing Methods for Helicopters

Undated

31 Report No. 157X90-1 Proposed Mechanical Stabilization for the Kaman H-43B Helicopter Kaman

Dec 29 1958

32 Report No. 66A-10-9 Theoretical Study of a Helicopter Rotor Employing Large Flapping Hinge Offsets; Aerodynamics Kellett

Feb 15 1954

33 Report No. R-598 Model K-120 Composite Helicopter Jul 30 1965

28

5

10

15

20

25

Brochure Kaman 34 Report No. LR 20807 Composite Aircraft Program

Retracted Rigid Rotor Lockheed-California Jul 1967

HELICOPTER ARTICLES AND PHOTOS 12 1 Helicopter History – Early Helicopters Photos & Articles Undated

2 Helicopter History – German Helicopters Articles Undated 3 Helicopter History – Germany 1939-1945 Articles,

Diagrams 1939-1945

4 Helicopter History – Historical Resume 1483-1954 Undated Bibliography of Rotary Wing Aircraft Undated

6 Helicopter History – Summary of Rotary Wing Projects of Aircraft Projects Section, Rotary Wing Branch

Jan 1947 – Feb 1947

7 Principles of the Helicopter by Dr. Alexander Klemin Articles

Undated

8 Helicopter Pamphlets/Photos Super Puma as332, ASTAR 350C, SA365 dauphin 2, UN-8B

Undated

9 AHS Semi Technical Bulletin Number 1 by James A. J. Bennett

May 1944

Helicopter History – 2 articles 1) Contemporary Helicopter Layouts; 2) From Rotorcraft Magazine – Specifications

1954

11 Lindenbaum Presentation to AHS The Autogiro in Prospective and Advanced Design Possibilities

May 2 1974

12 Helicopter History – Miscellaneous Articles, Proposals and Photos

Undated

13 Helicopter Transparencies for The Helicopter – A Historical Perspective – by Lindenbaum

Sep 15 1981

14 Journal of the AHS Volume 1, Number 1 Jan 1956 Helicopter Pilot’s Aerodynamic Outline – Bell Helicopter Training School

1951

16 Helicopter History – BELL Photos Undated 17 Military Products Reference Data – BELL Undated 18 Helicopter History – BELL Pamphlets and Photos Undated 19 Helicopter History – BOEING VERTOL Pamphlets and

Photos Undated

Helicopter History –BOLKOW Helicopter Articles and Pamphlets

Undated

21 Helicopter History – CESSNA Yh-41 Photo Undated 22 Helicopter History – DOMAN Articles and Photos Undated 23 Helicopter History – DORNIER (German)Photos Undated 24 Helicopter History – FI RESTONE Photos Undated

Helicopter History – FOCKE (German)Photo Undated 26 Helicopter History – GYRODYNE Photos Undated 27 Helicopter History – HILLER Photos and Newsletter Nov 1969

28 Helicopter History – HUGHES Articles, Photos and Undated

29

Pamphlets 29 Helicopter History – KAMAN Photos and Articles Undated 30 Helicopter History – KAMOV (Russian) Photos and

Articles Undated

31 Helicopter History – KELLETT Photos Undated 32 Helicopter History – LANDGRAF Article and Photo 1944 33 Helicopter History – LOCKHEED Pamphlet and Photo Undated 34 Helicopter History – McCULLOCH MOTORS Proposals

MC-9 Helicopter 1952

35 Helicopter History – McDONNELL (early) Photos Undated 36 Helicopter History – MIL (Russian) Articles Undated 37 Helicopter History – PIASECKI Photos Undated 38 Helicopter History – PLATT-LEPAGE Photos Undated 39 Helicopter History – SEIBEL Photo Undated 40 Helicopter History – YAK and ANTONOV Articles 1961

13 1 No. X-417-13 Model Specification for Army Air Forces Helicopter Model YR-1A (Manufacturer’s Model PL-7) Platt LePage

Jan 16 1945

2 FT-56R-67 AD820490 Naval Air Test Center TR Final Report Evaluation of the Bell Model 206A(Jetranger) Light Turbine-Powered Helicopter

Sep 14 1967

3 No. X-417-14 Rotary Wing Aircraft Specifications Vol. II AAF Model XR-6A

Feb 20 1945

4 McDonnell Model 4JP2-MD-5 Blueprints Aug 19 1957 5 Report 5930A Model Specification Helicopter Final

Corrected data Model XR-5 Contract# W535 ac-29845 and DA W535 ac-2514 Sikorsky

Dec 1 1944

6 Report SER-130 Model Specification Helicopter (Tentative) Model YR-5C Contract#W535 ac-41023 Sikorsky

Mar 22 1945

7 Report SER-499A Model Specification Helicopter Model R-5D Contract# W535 ac-41023 Sikorsky

Feb 20 1947

8 Report SER-257 Airplane-Helicopter AAF Model R-5F Sikorsky

Dec 12 1946

9 AF TR No. 6163 XH-10 Helicopter Development of Kellett Model

May 1950

10 Report SER-1556 Model Specification Helicopter Model E-5G Sikorsky

Nov 22 1948

11 Report 204-947-030 Detail Specification for H-40A Utility Helicopter Bell

Jan 10 1957

12 Report 54-947-001 Model Specification XR-15 Bell May 22 1946 13 Report SER-3309 Detail Specification, Model H-19D

Helicopter, 12-Place, Single Engine – Sikorsky Nov 17 1953

14 Report SD-530-1-6 Detail Specification for Model UH-2B FY 1964

30

(HU2K-1U) 15 Sikorsky Contractor Technical Compliance Conference

Model H-34A Helicopter Jan 24-26 1955

16 Report SD-516-1 Detail Specification for Model HUL-1 Helicopter Class HU (Single Engine) Contract# NOas 55­485

Mar 22 1955

17 Model XH-3 Blueprints Higgins Sep 28 1945 18 Report 133 Detail Specification for Design and

Construction of H-3 Helicopter Higgins Sep 27 1945

19 Report R-100 Model Specification Helicopter Model X-2A Rotor-Craft Corp.

Mar 14 1945

20 Report 57-123 Detail Specification for Model XROE-1 Rotorcycle Class RO Hiller Helicopter

Undated

21 Report SD-511 Detail Specification for Model XROE-1 Rotorcycle Class RO Contract# NOas 55-387c

Sep 29 1954

22 Report S-157-b Model Specification, Model XH-26 Single-Place Helicopter Contract# AF33(038)-27961

Jun 8 1951

23 Development of the XH-26 Helicopter Sep 1956 24 NASA TN D-3060 Flight Tests of the One Man Helicopter

and a Comparison of Its Handling Qualities with Those of Larger VTOL Aircraft

Oct 1965

25 XH-26 Development Engineering Inspection Sep 15-16 1953 26 The XA-5 Pulse Jet Powered Helicopter Jun 1 1950 27 The Pinwheel Rocket Propelled Strap on the Back

Helicopter Rotor-Craft Presentation Undated

28 Gyrodyne Reconnaissance/Surveillance Drone, Model QH­50C Letter with Attached Brochure

May 7 1965

29 Report PTR AC-4031 Contractor’s Part II Structural and Aerodynamic Demonstration of Goodyear Model GA400R-3J One Man Helicopter, Report no. 1 Final Report

Apr 26 1957

30 Hughes 500 Helicopter Brochure Undated 31 Report 22-X-201 Rev. C Model Specifications H-21B

Helicopter Piasecki Mar 16 1951

32 Detail Specification for Model HUP-2 Helicopter Class HU Single Engine, Twin Rotor Contract# NOas 51-035

Nov 19 1951

33 NAVAER SD-418 Detail Specification for Model XHJP-1 Helicopter Class HJ (Twin Rotor) Contract# NOa(s)-7935

Mar 4 1946

34 Report 190-1 Specification for Model 190 Helicopter Hughes

Apr 5 1951

35 Report SD-363-2 Detail Specification for Model HRP-2 Helicopter Class HR (Twin Rotor) Contract# NOa(s) 9978

Jun 21 1948

36 Report SER-5004 Detail Specification, Model H-19D Helicopter, 12-Place, Single Engine Contract#AF33(600)­33862 Sikorsky

Jun 29 1956

37 HC-65A-1 Mechanical Description and Aerodynamic Dec 5 1950

31

Analysis Heli-Craft, Ltd. 38 Report MCRFT-2270 Phase II Flight Tests of the Sikorsky

H-5H Helicopter Mar 10 1950

39 Helicopter (unnamed) Configuration Drawings with Boeing 502-10C Gas Turbine

Undated

40 Report 161518 and 161523 CIRCOL OFFLINE OUTPUT 3 reports

Aug 1972

41 HUL-1 Drive Assembly Blueprints Bell Mar 18 1955 42 Report SER-2556 Summary Report Long Range

Helicopter Design Study Contract AF33(616)-2628 Two Copies

May 27 1955

43 Report SER-2553 Long Range Helicopter Results and Analyses Compound Helicopter Configuration

May 16 1955

44 NAVWEPS 01-260HCA-2-4 Handbook Maintenance Instructions Navy Model HU2K-1 Helicopter – Transmission System

Dec 1 1961 rev Jul 1 1962

45 WADC TR 55-468 General Design Study of Performance Improvement of Helicopters

Jan 1956

46 KAMAN Aircraft Annual Report 1956 1956 47 Monte-Copter, Inc. Press Release/Brochure Jan 13 1966 48 NAVWEPS 01-260HCA-2-5 Handbook Maintenance

Instructions Navy Model UH-2A/UH-2B(HU2K-1) Helicopter – Rotor System

Oct 15 1962 rev Feb 1 1963

49 Model QH-50C Drone Description and Capabilities Gyrodyne

Sep 17 1964

50 Boeing-Vertol Model-137 Dynamics Jan 27 1961 51 Boeing-Vertol Model-137 Power Plant Analysis Jan 27 1961 52 Boeing-Vertol Model-137 Reliability Jan 27 1961 53 Grumman Design 242 Tri-Service VTOL Aircraft Proposal

Drawings Apr 3 1961

54 Grumman Design 242 Tri-Service VTOL Aircraft Carrier Design Compromises

Apr 3 1961

14 1 Military Products Reference Data Bell Helicopter Oct 1 1973 2 Report ADR-01-03-61.1 Aerodynamic Design & Stability

Analysis of a Rotating Wing Towed Glider Grumman Aug 1961

3 AFFTC-TR-60-2 Appendix III YHO-2HU Air Force Flight Evaluation

May 1960

4 Report No. 130-13 A Chart Method for Calculating Helicopter Performance – II Kellett

Nov 1946

5 Rocket Propeller Mini-Copter C.A. 1975 6 Report 22-A-05 Report on Methods and Computations

Used in Selecting Rotor Physical Characteristics and Efficiencies for the H-21 Helicopter Contract# AF33(038)­12881 Piasecki

Apr 1951

7 Report 42-A-03 H-21B & C Helicopter Rotor Blade Dec 11 1951

32

Airload Report Contract# AF33(038)-12881 Piasecki 8 Report 22-S-41 Control System Analysis – Rotor

Contract# AF33(038)-12881 Piasecki Jan 15 1952

9 Report 42-S-10 H-21B & C Rotor Blade Stress Analysis Contract# AF33(038)-12881 Piasecki

Feb 13 1952

10 WADC TR 52-256 Low-Range Air-Speed Indicator for Helicopters

Oct 1952

11 Report MCREXB-582-7-2 Stress Survey of Sikorsky H-5 Main Rotor Blades

Jan 19 1949

12 Report SER-246 Preliminary Experimentation Single Blade Rotor Model Sikorsky

Apr 7 1945

13 Nagler Rocket Rotor System 1951 14 Presenting the Firestone Helicopter 1946 15 Proposal 157-7 Description of Container for the Aerial

Delivery of the XH-26 Collapsible Helicopter Jan 25 1952

16 Bell H-13 Helicopter Brochure Undated 17 American Helicopter Model 175 brochure Undated 18 Air Material Command Letters (5) 1947-1950 19 McCulloch Motors Proposal – R&D Projects Feb 24 1953 20 Blueprint Packet KAMAN Helicopter 1947 21 Helicopter Research Laboratory Blueprints and Notes –

Lindenbaum 1947

22 Helicopter Material – General File – Lindenbaum Undated 23 Miscellaneous Blueprints C.A. 1945 24 Flight within Earth’s Atmosphere May 16-18 1966 25 AIAA Paper No. 69-199 Research and Development of

Advanced Rotorcraft Concepts by Evan A. Fradenburgh Sikorsky

Feb 17-19 1969

26 Multivariable Search and Its Application to Aircraft Design Optimization by W.Z. Stepniewski & C.F. Kalmbach, Jr. Boeing-Vertol

Sep 15 1969

27 Present and Future Roles of the Helicopter by L.L. Douglas & J.J. Schneider Boeing-Vertol

May 1965

28 The Piasecki Story of Vertical Lift Undated 29 An Investigation into the Rotor Torque Problem of the

Hafner Helicopter Sep 1938

30 Specification – Hafner Helicopter P.D.6 Sep 1938 31 Specification – Hafner Helicopter P.D.7 Sep 1938

HELO PHOTOS, BROCHURES 15 1 Box of Photos Undated

2 AIAA Symposium – Evolution of Aircraft Wing Design Mar 18-19 1980 3 Charts – Rotary Wing 1934-1946 4 Airplane Charts & Data C.A. 1944 5 Photos – Early Helicopters Various 6 Helicopter Photos and Articles Various

33

7 Advancing Blade Concept 1966 8 CH-53E Super Stallion Brochure Sikorsky Undated 9 Sikorsky UTTAS Brochure Oct 1975 10 Sikorsky 76 Brochure Undated 11 Helicopter Articles Various 12 Helicopter Brochures Various 13 R-4 First Landing on Ship (Photos) Undated 14 Theory of Flight of Sikorsky Helicopters Jan 16 1953 15 AHS Quarterly Vol. 1 No. 1 Jan 1946 16 Pilot Operating Instructions for 1) R-5A/HO2S-1 and 2) R­

6A and HOS-1 1944-1945

17 General Comments on Sikorsky R-4, R-5, R-6 Helicopters Dec 18 1945 18 Report NO. X-417-13 Rotary Wing Aircraft Specifications

Vol. I (Model YR-1A) Platt-LePage Jan 16 1946

EARLY HELICOPTERS & TOWED HELICOPTERS 16 1 Report No. TB-641-F-1 Transient Responses of an H-13

Helicopter to Longitudinal Stick Pulses as Measured in Flight Cornell

Nov 15 1950

2 Kaman K-800 Brochure Undated 3 Report No. FTC-TIM-68-1006 Helicopter Range/Speed

Extension, Mother-Daughter Approach May 1968

4 Report of Helicopter Aerial Tow Accident of Aug 25 1950 with Photos

Oct 6 1950

5 Powered Long Line Loiter System (POLLLS) documents and Photos Aerial Mobility Inc.

1994

6 Report No. 55McC103R Full Scale Investigation of Rotor Hub Fairing for a Sikorski H-5 Rotor Hub Contract# AF 18(600)-176

Apr 1955

7 Effects of Operating and Design Variables on Helicopter Performance by Alfred Gessow

Jan 27 1949

8 Helicopter Brochures Undated 9 Mechanical Description and Aerodynamic Analysis of

Model HC-65A Helicopter Utility Metal Products, Inc. Jul 16 1954

10 MI-26 Halo as Viewed by an American Presentation Jan 20 1997 11 AFFTC-TR-59-41 High Altitude Take-Off and Landing

Tests of the H-37A Equipped with Narrow Chord Blades Dec 1959

12 The de Bothezat Helicopter Articles and Photos C.A. 1922 13 Flight Within Earth’s Atmosphere – VTOL Aircraft 1975­

1985 Briefing Boeing-Vertol May 16-18 1966

14 Specification – Hafner Gyroplane A.R.4 Sep 1938 15 Report No. SER-1775 Tow Tests of H-5 (S-51) Helicopter

Contract# AF 33(038)-7878 Oct 19 1950

16 Report of Test Project NR AVN 5258/59(D) Desert Test of the YHO-2HU Helicopter

Oct 14 1959

17 Performance Substantiation for Kinedyne Proposal Cessna Feb 5 1958

34

18 Comparative Evaluation of the Kinedyne 1958 19 Proposal Model CH-3 Kinedyne Apr 21 1958 20 AHS 13th Annual Forum Theoretical and Experimental

Study of the Coupled Flap Bending and Torsion Aero-Elastic Vibrations of a Helicopter Rotor Blade by Peter F. Leone Vertol

May 8-10 1957

21 H-5D Helicopter Aerial Tow Tests Letter Oct 25 1948 22 Report No. E-57-1065 Flight Evaluation of the Bell Model

47G-2 Hiller Sep 9 1957

23 MIL-S-8698(ASG) Structural Design Requirements, Helicopters

Aug 1 1950

24 Report No. 127A90-4 The Effects of Airframe Shape on Helicopter Performance and Stability Contract# AF 33(616)-5420 Kellett

Jul 31 1958

25 Report No. D34-947-001 Specification for Single Engine Two Bladed helicopter Bell

Sep 29 1945

26 Report SER-257 Model Specification – Helicopter R-5F Sikorsky

Dec 12 1946

27 AHS Western Forum Air Force Test Experience with Turbine Powered Helicopters by James S. Hayden AF Flight Test Center

Sep 25-26 1958

28 AFFTC-TR-59-33 YH-40 Performance Evaluation Jan 1960 29 Introduction to Helicopter Aerodynamics Vol. 1 –

Performance by W.Z. Stepniewski Piasecki 1950

30 Report No. SER-86 Description of Sikorsky Experimental Blades Contract W535 AC-41023 Sikorsky

Mar 13 1945

31 Final ER on Various Helicopter Rotor Tip[-Path Plane Data and Transmission Systems Contract# NOas 54-485C

1955

32 AFFTC-TR-60-57 HU-1 Stability and Control Evaluation Dec 1960 33 Wirtschaftlichkeit des Hubschrabers by W. Lambert, E.

Skubinna & H. Brusberg (in German) Sep 1959

34 Lateral-Directional Stability and Control of Helicopters. Effect of Design Parameters by W. Just, H. Georgi & U. Schwellinger

1958-1959

35 Helicopter – Miscellaneous Various 36 Project No. PTR AD 3097 Navy Evaluation of the Model

YHC-1A Helicopter Report No. 1 Final Report May 5 1960

37 USAAVLABS TR 69-78 A Flight Envelope Expansion Study for the XH-51A Compound helicopter

Oct 1969

38 WADC TN 59-88 YH-40 (UH-1) Helicopter Extreme temperature Arctic Evaluation

Aug 1959

39 WADC TR 55-438 The Determination of Helicopter Longitudinal Stability Derivatives from Flight Test Data Part III Contract AF 33(616)-5361

Sep 1959

17 1 NASA TR R-41 Normal Component of Induced Velocity 1959

35

for Entire Field of a Uniformly Loaded Lifting Rotor with Highly Swept Wake as determined by Electromagnetic Analog

2 NASA TR R-71 Jet-Boundary Corrections for Lifting Rotors Centered in Rectangular Wind Tunnels

1960

3 NASA TT F-43 A Vibration Absorber for Two-Bladed Helicopters (from French)

Nov 1960

4 NASA TT F-55 Response of a Helicopter Rotor to an Increase in Collective Pitch for the Case of Vertical Flight (from French)

Jan 1961

5 NACA TN 2870 Power-Off Flare-Up Tests of a Model helicopter Rotor in Vertical Autorotation

Jan 1953

6 NASA TN D-31 A Dynamic Model Investigation of the Effect of a Sharp-Edge Vertical Gust on Blade Periodic Flapping Angles and Bending Moments of a Two-Bladed Rotor

Sep 1959

7 NASA TN D-43 An Evaluation of Linearized Vortex Theory as Applied to Single and Multiple Rotors Hovering in and Out of Ground Effect

Sep 1959

8 NASA TN D-58 The Effect of Various Combinations of Damping and Control Power on Helicopter Handling Qualities During Both Instrument and Visual Flight

Oct 1959

9 NASA TN D-186 A Flying-Qualities Study of a Small Ram-Jet Helicopter

Apr 1960

10 NASA TN D-245 Compressibility Effects on the Hovering Performance of a Two-Bladed 10-Foot-Diameter Helicopter Rotor Operating at Tip Mach Numbers up to 0.98

Apr 1960

11 NASA TN D-251 A Summary of Operating Conditions Experienced by Two Helicopters in a Commercial and a Military Operation

Apr 1960

12 NASA TN D-335 Full-Scale Wind-Tunnel Tests of Blowing Boundary-Layer Control Applied to a Helicopter Rotor

Sep 1960

13 NASA TN D-382 Effects of Blade Cut-Out on Power Required by Helicopters Operating at High Tip-Speed Ratios

Sep 1960

14 NASA TN D-393 Measurements of the Time-Averaged and Instantaneous Induced Velocities in the Wake of a Helicopter Rotor Hovering at High Tip Speeds

Jul 1960

15 NASA TN D-394 Equations for the Induced Velocities Near a Lifting Rotor with Nonuniform Azimuthwise Vorticity Distribution

Aug 1960

16 NASA TN D-432 A Summary of Operating Conditions Oct 1960

36

Experienced by Three Military Helicopters and a Mountain-Based Commercial Helicopter

17 NASA TN D-458 Experimental Smoke and Electromagnetic Analog Study of Induced Flow Field About a Model Rotor in Steady Flight Within Ground Effect

Aug 1960

18 NASA TN D-464 Effects of Control-Response Characteristics on the Capability of a Helicopter for Use as a Gun Platform

Sep 1960

19 NASA TN D-534 Hovering Measurements for Twin-Rotor Configurations with and Without Overlap

Nov 1960

20 NASA TN D-633 An Analysis of the Flapwise Bending Frequencies and Mode Shapes of Rotor Blades Having Two Flapping Hinges to Reduce Vibration Levels

Dec 1960

21 NASA TN D-742 Hovering Characteristics of a Rotor Having an Airfoil Section Designed for Flying-Crane Type of Helicopter

Apr 1961

22 NASA TN D-737 Some Recent Studies in Structural Dynamics of Rotor Aircraft

Mar 1961

SERIES V: Helicopter Aerodynamics, 1918-1993

Box File Description Date

HELICOPTER AERODYNAMICS AND THEORY 18 1 TSEAL-2-4202-2-23 Calculated Directional Stability

Characteristics of XR-8 Helicopter Contract# W535 ac­40711

20 Mar 1945

2 Report No.ENG-6838 Chart Method for Calculating Helicopter Performance Project MX-558 Kellett

16 Jan 1945

3 UAAAMRDL TR 72-16 An Analytical Evaluation of the Controllable Twist Rotor Performance and Dynamic Behavior Contract# DAAJ02-67-C-0068

May 1972

4 The Boundary Layer and Skin Friction for a Figure of Revolution at Large Reynolds’ Numbers –Article – Dr. Norton B. Moore

1935

5 NACA TN-2318 Full Scale Tunnel Investigation of the Static-Thrust Performance of a Coaxial Helicopter Rotor

Mar 1951

6 NACA TN 3236 Wind-Tunnel Studies of the Performance of Multirotor Configurations

Jun 1954

7 Report ACR No. L4H07 Charts for Estimation of the Characteristics of a Helicopter Rotor in Forward Flight I-Profile Drag-Lift Ratio for Untwisted rectangular Blades

Aug 1944

8 Report ACR No. L5E04 Charts for Helicopter Performance Estimation

Aug 1945

9 NACA Report No. 538 Altitude-Pressure Tables Based on 1942

37

the United States Standard Atmosphere 10 Report No.SC-4139(TR) Stability of an Aerodynamic

Body with a Rotor Dec 1957

11 NACA TN 2665 An Extension of Lifting Rotor Theory to Cover Operation at Large Angles of Attack and High Inflow Conditions

Apr 1952

12 NACA TN 3323 Charts for Estimating Performance of High-Performance Helicopters

Jan 1955

13 NACA TN 3482 Supplementary Charts for Estimating Performance of High-Performance Helicopters

Jul 1955

14 Report No. FT-67R-67 NATC Evaluation of the Hughes OH-6A (Cayuse) Light Turbine-Powered Helicopter

Oct 17 1967

15 TM 816 The Gyroscope – Its Principles and Its Possibilities by Louis Breguet

Jan 1937

16 Historic Rotorcraft – Kellett Collection Oct 17 1954 17 Helicopter Fundamentals by Wayne Wiesner Jan 1955 18 NACA Report No. 20 Aerodynamic Coefficients and

Transformation Table 1918

19 NACA Report No. 311 Aerodynamic Theory and Test of Strut Forms

1929

20 NACA Report No. 335 Aerodynamic Theory and Test of Strut Forms – II

May 1929

21 NACA Report No. 716 A Simplified Theoretical Method of Determining the Characteristics of a Lifting Rotor in Forward Flight

1941

22 Biological and Aerodynamic Problems of Animal Flight Article by Erich von Holst & Dietrich Kuchemann

Jun 13 1941

23 Results from the Deutsche Forschungsanatalt Fur Segelflug Smoke Tunnel Article by A. Lippisch

Dec 15 1938

24 NACA TN 4409 Flight Measurements of the Vibration Experienced by a Tandem Helicopter in Transition, Vortex-Ring State, Landing Approach and Yawed Flight

Sep 1958

25 Introduction to Rotorcraft Part I & II by Franklin D. Harris 1994 26 Role of the Rotary Wing in Future Short-Haul

Transportation Pamphlet Lockheed Undated

27 NASA TN D-4820 A Hovering Investigation of an Extremely Flexible Lifting Rotor

Oct 1968

28 Sketch of Hiller 12C Helicopter Undated 29 Report No. R-700 Analytical Study to Determine Optimum

Design Criteria of Non-Servo Flap Controlled Rotors Contract# Now 64-0488f Kaman

Jun 1967

30 Report No. FFA 123 Disk Approximation for a Helicopter Rotor in Forward Flight

1972

31 Report No. 065298 CIRCOL OFFLINE OUTPUT – General Design of the Dornier Tail Rotor System

Aug 24 1973

32 FSTC-HT-23-480-72 Autorotation of Coaxial Helicopters Aug 24 1972

38

Translation (from Russian) 33 FSTC-HT-23-1174-01 Light Turbine Helicopter DO-123

Translation (from German) Dec 14 1972

34 FSTC-HT-23-107-73 On Cause of Vibrations in Helicopters translation (from German)

Aug 16 1973

35 Report AFFDL-TR-69-113 A Method for Calculating Helicopter Vortex Paths and Wake Velocities

Jul 1970

36 NASA CR-1672 Nonlinear Actuator Dick Theory and Flow Field Calculations, Including Nonuniform Loading

Sep 1070

37 Cessna CH-1 Helicopter Pamphlet Undated 38 Report No. EX-0-2 Studies Relative to the Development of

a One-Man Helicopter Part II Performance, Flying Qualities, Powerplants and Fuels Contract# Nonr 611(00) Amendment 1

Jan 20 1954

39 Report No. 47-947-039 Detail Specification for Bell Model 47J Four Place Helicopter

Sep 1 1955

40 Development of the OH-6A for Maximum Performance and Efficiency

May 13-15, 1964

41 US Army OH-6A Pamphlet Undated 42 Presenting the Firestone Helicopter Pamphlet Undated 42 Report No. EX-0-1 Studies Relative to the Development of

a One-Man Helicopter Part I Contract# Nonr 611(00) Amendment 1

Sep 30 1953

44 Proposal for a Multi-Purpose Turbine Powered Helicopter Model 1082 Pamphlet Hiller

Jan 1958

45 Report No. 55-77 Two Place Observation Helicopter Preliminary Design Study Contract# DA 44-177-TC-421 Hiller

Aug 1957

46 Report No. AU-74 Revision A Helicopter Model Specification 1 Place, Single Engine, Liaison Type Model GA-45B (XR-9) Contract# W-33-038-1708

Dec 20 1943

47 Report No. 63-35 A proposal for a Twin-Engine, High-Performance, Light Observation Helicopter OH-5B

Apr 1963

48 ABC(Advanced Blade Concept) Meeting at ARPA (Advanced Research Projects Agency) Notes

Mar 1971

49 Helicopter Medical Evacuation Techniques at Toulouse Hospital Trip Report

Jul 11 1969

50 Optimization of Design Data for Reaction Drive Helicopters Translation (from German)

Jan 1970

51 FSTC-HT-23-1269-72 Method of Decreasing Vibration in Rotary Wing Aircraft Translation (from Russian)

Jun 19 1972

52 Report No. 8011-099-002 The Weights of Very Large Rotors for Nuclear Powered Helicopters

Apr 23 1959

53 Report No. FTC-TR-69-6 Slope Landing Tests with the CH-3E Helicopter

Apr 1969

54 Report No. 150-P-1006P Proposal to Establish the Weight Jan 1973

39

of a Large Reaction Drive Helicopter Hughes 55 Optimum Pitch Rotor Presentation Hughes Undated 56 Sikorsky S-67 Blackhawk Article Fall 1970 57 Your Flight in the Lockheed Rigid Rotor Helicopter Undated 58 SA 341 Gazelle Helicopter Brochure c.a. 1968 59 Helicopter Pamphlets (Brantley, Kaman, Hughes, Bell,

Boeing, Vertiflite) (13 items) Undated

60 Planning Purpose Proposal for Developmental Research of the Lockheed ABIL (Automatic Blowing Inducted Lift) Rotor

Oct 14 1969

61 Investigation of CH-3E Reynolds Number Effects and Gross Weight/Pressure Ratio Test Techniques

Dec 1968

62 State of the Art Advancement in Helicopter Design (Rigid Rotor) Lockheed

Undated

63 1969 IR&D Studies Aerodynamic Research Rotor Performance Methodology

1969

64 The Helicopter Rotor at High Mach Numbers May 10-12, 1967 65 Rotary Wing Boundary Layer and Related Researches Sep 11-13, 1967 66 Variable Deflection Thrust (VDT) Fluidically Controlled

Rotor System Honeywell 9D-F-1 Mar 13 1969

67 Development of the Kinematic Focal Isolation System for Helicopter Rotors Bell

May 1968

68 Fairchild Hiller 68-4 Reverse Velocity Rotor Task Undated 69 Fairchild Hiller Reverse Velocity Rotor Task 7 Documents 1968 70 Fairchild Hiller 68-7 Desensitized Rotor System Study

Volume I Dec 31 1966

71 Report No. R-846 The Effects of Material Properties on Helicopter Rotor Blade Frequencies

Mar 1970

72 The Flapping/Feathering Ratio of a Second Harmonic Input for an 8 Foot Diameter 4 Blade Articulated Rotor

Apr 24 1972

18A 1 HTC-AD 72-57 150-A-1005P Proposal for Optimum Pitch Rotor System – Analysis and Wind Tunnel Model Program Hughes

Jun 1972

2 HTC-AD 72-57 Supplementary Information to the OPR Proposal for Analysis and Wind Tunnel Model program Hughes

Jul 1972

3 HTC-AD-72-57 150-A-1005P Part II Supplemental Information to the OPR Proposal for Analysis and Wind Tunnel Model Program Hughes

Undated

4 RPV – OPR Remote Piloted Vehicle with Optimum Pitch Rotor System

Mar 1973

ROTORS, AHS FORUM REPORTS

40

19 1 Report No. 360.1 Transport Helicopter Operating Cost Analysis Methods Contract# Nonr-1340(00)

Nov 30 1955

2 26th Annual National Forum of the AHS– An Investigation of the Need for Improved Displays in Heavy-Lift Helicopters by Archie T. Sherbert Jr, - Boeing-Vertol

Jun 1970

3 27th Annual National V/STOL Forum of the AHS– A Method for Predicting Helicopter Wake Geometry, Wake-Induced Flow and Wake Effects on Blade Airloads by S.G.Sadler – Rochester Applied Science Assoc.

May 1971

4 27th Annual National V/STOL Forum of the AHS– Tip Vortices – Velocity Distributions by N.A.Chiger & V.R.Corsigia – NASA Ames

May 1971

5 27th Annual National V/STOL Forum of the AHS– Rotor Stability Derivatives Determined From Wind Tunnel Tests of an Instrumented Helicopter by Robert E. Rohtert & Sally V. LaForge – Hughes Tool, Aircraft Div.

May 1971

6 27th Annual National V/STOL Forum of the AHS – HLH Primary Flight Control System Design by Richard W. Sanford, Peter R. Venuti & Derek Wood – Boeing-Vertol

May 1971

7 27th Annual National V/STOL Forum of the AHS – Application of a Lifting-Surface Theory to the Calculation of Helicopter Airloads by Wayne Johnson – MIT

May 1971

8 27th Annual National V/STOL Forum of the AHS – A Study of the Effects of Nonuniform Swash-Plate Stiffness and Out-of-Blade Track on Rotor Dynamics and Stability by Vincent J. Piarulli – Rochester Applied Science Assoc.

May 1971

9 27th Annual National V/STOL Forum of the AHS – The Method of Multiblade Coordinates in a Linear Analysis of Lifting Dynamic Stability and Gust Response at High Advance Ratio by Sheng-Kuang Yin & Kurt H. Hohenemser – Washington Univ.

May 1971

10 27th Annual National V/STOL Forum of the AHS – Prediction of Control Loads Due to Blade Stall by F.J. Tarzanin, Jr. - Boeing-Vertol

May 1971

11 27th Annual National V/STOL Forum of the AHS – Preliminary Development of an Active Transmission Isolation System by Paul W. vonHardenberg & Paul B. Saltanis – Sikorsky

May 1971

12 27th Annual National V/STOL Forum of the AHS – Analytical Investigation of the Effects of Blade Flexibility, Unsteady Aerodynamics, and Variable Inflow on Helicopter Rotor Stall Characteristics by E.D. Bellinger – United Aircraft

May 1971

13 27th Annual National V/STOL Forum of the AHS – May 1971

41

Detailed Aerodynamic Measurements of a Model Rotor in the Blade Stall Regime by Richard K. Fisher, Jr. & W.J. McCroskey – Boeing & USArmy Air Mobility R&D Lab

14 27th Annual National V/STOL Forum of the AHS – Feel Augmentation and Sensitivity Control in High Speed Helicopters by Sean J. O’Connor - Sikorsky

May 1971

15 27th Annual National V/STOL Forum of the AHS – An Attack Helicopter Weapons Delivery System by John A. Simpson – United Technologies/Norden Division

May 1971

16 27th Annual National V/STOL Forum of the AHS – Head-Mounted Display/Control System in V/STOL Operations by Dr. Dora Dougherty & Hubert W. Upton – Bell Helicopters

May 1971

17 27th Annual National V/STOL Forum of the AHS – Day and Night Fire Power of the Cheyenne by Bernard J. Merritt & John C. Kirby – USAMC & Lockheed-Burbank

May 1971

18 27th Annual National V/STOL Forum of the AHS – The Night Rescue Terminal Navigation Problem by Cecil S. Richardson – Sikorsky

May 1971

19 27th Annual National V/STOL Forum of the AHS – Army Helicopter Performance Trends by Richard B. Lewis – USArmy Aviation Systems Test Activity

May 1971

20 27th Annual National V/STOL Forum of the AHS – The Boeing Model 347 Advanced Technology Helicopter Program by Frank H. Duke & W. Euan Hooper – Boeing-Vertol

May 1971

21 27th Annual National V/STOL Forum of the AHS – Strain Gauge Torquemeters for Use in Helicopter Transmission Systems by Dennis P. Hames – British Hovercraft Corp.

May 1971

22 27th Annual National V/STOL Forum of the AHS – Evaluation of Rotor Controls Designed for Increased Safety by Lawrence D. Barrett & John C. Mack – Boeing-Vertol

May 1971

23 27th Annual National V/STOL Forum of the AHS – Fail-Safety for the H-46 Rotor Blade by George H. Thompson & William L. Weiss – Boeing-Vertol

May 1971

24 27th Annual National V/STOL Forum of the AHS – Fatigue Strength Improvements in Ti-6A1-4V Forgings by John J. Lucas – Sikorsky

May 1971

25 27th Annual National V/STOL Forum of the AHS – AN/ASN-86 Inertial Navigation Set by J. B> Hughes – Litton Ind.

May 19-21 1971

26 Factors Affecting Fuel Control Stability of a Turbine Undated

42

Engine/Helicopter Rotor Drive System by C. Fredrickson, K. Sumford & C. Stephenson – Boeing-Vertol, AVCO/Lycoming & AVSCOM

27 TR AFFDL-TR-69-113 A Method of Calculating Helicopter Vortex Paths and Wake Velocities Air Vehicle Corp.

Feb 1970

28 26th Annual National Forum of the AHS – Collection and Analysis of Helicopter Combat Flight Loads Data from AH-1G Helicopters in Southeast Asia by F. Joseph Giessler & William T. Alexander – Technology Inc. & USArmy Aviation Materials Lab

Jun 1970

29 26th Annual National Forum of the AHS – The CH-47 Cruise Guide Indicator by W.P. Brown & H.H. Steinmann – Boeing-Vertol

Jun 1970

30 26th Annual National Forum of the AHS – Qualitative Report on Flight Test of a Two-Point External Load Suspension System by A.J. Hutto – Boeing-Vertol

Jun 1970

31 CAL Report BB-2584-S-1 On the Feasibility of Replacing a Helicopter Tail Rotor Contract# N00014-68-C-0241 NR212-182

Jul 1968

32 USAAVLABS TR 69-18 Measurement of Rotor Noise Levels and Evaluation of Porous Blade Tips on a CH-47A Helicopter Contract# DA 44-177-AMC-330(T)

Sep 1969

33 NASA TN D-742 Hovering Characteristics of a Rotor Having an Airfoil Section Designed for Flying-Crane Type of helicopter

Apr 1961

34 NASA TN D-1517 Hovering Characteristics of a Rotor Having an Airfoil Section Designed for a Utility Type of Helicopter

Dec 1 1962

35 5th Annual National Forum of the AHS – Design and Construction of the Cornell Fiberglass Helicopter Main Rotor Blades by Harold Hirsch – Cornell Aeronautical Lab.

May 12-13, 1949

36 AHS – Great Lakes regional Dinner Meeting Three (3) ARTICLES: 1) Results of Recent Rotor Blade De-Icing Test on Mt. Washington, Part I by Lt. Comdr. L. Carson Houser – USN Bureau of Aeronautics; 2) Results of Recent Rotor Blade De-Icing Test on Mt. Washington, Part II by Robert R. Lynn – Bell; 3) Helicopter Maneuver Loads in Relation to Recent Specifications and Tests by O. Q. Niehaus – Bell

Jan 7 1952

37 USAAVLABS TR 70-47 Analysis of Measured Helicopter Rotor Pressure Distributions Contract# DAAJ02-69-C­0076

Sep 1970

38 NASA TN D-734 Considerations of Methods of Improving Apr 1961

43

Helicopter Efficiency 39 NASA TN D-759 Flight Investigation of Effects of

Selected Operating Conditions on the Bending and Torsional Moments Encountered by a Helicopter Rotor Blade

Apr 1961

40 FTC-TR-66-46 Determination of the Effects of Rotor Blade Compressibility on the Performance of the CH-47A Helicopter

Mar 1967

41 Report No. SG-1195-S-2 A Proposed Test Apparatus For Small Rotorcraft Vol. II Contract# DA-44-177-TC-440

Apr 1958

42 NASA TN D-458 Experimental Smoke and Electromagnetic Analog Study of Induced Flow Field About a Model Rotor in Steady Flight Within Ground Effect

Aug 1960

43 NASA TN D-534 Hovering Measurements for Twin-Rotor Configurations with and without Overlap

Nov 1960

44 NASA TT-F-43 A Vibration Absorber for Two-Blased Helicopters (translated from French)

Nov 1960

45 AMC F-TS-687-RE Stability in Hovering of the Helicopter with Central Rotor Control (Tr. From German)

Aug 1946

46 AMC F-TS-690-RE Contributions to the Dynamic Stability of Rotary-Wing Aircraft with Articulated Blades (tr. From German)

Aug 1946

47 AMC F-TS-692-RE The Pull-Up of the Helicopter (tr. From German)

Aug 1946

48 AMC F-TS-1002-RE The Dynamic Stability of Helicopters with Articulated Blades (Tr. From German)

Sep 1946

49 AMC F-TS-1004-RE The Theory of the Control of the Blade Angle of the Helicopter (Tr. From German)

Sep 1946

50 AMC F-TS-1006-RE Theory of Helicopter Control in Hovering Flight (Tr. From German)

Sep 1946

51 Report No. 179T80-2 An Investigation of VTOL Operational Problems Due to Downwash Effects Contract# Now 60-0450-f Kellett

Jun 12 1961

52 Report No. 20280-1 Proposal for the Study and Development of Design Criteria for High Speed Power Transmission Shafts Kellett

Jan 19 1961

53 Report No. 120X-10-1 Proposal – An Analytical Determination of an Optimum Rotor Blade Twist and Tip Speed for High Performance Helicopters Kellett

Feb 25 1957

54 Report No. 140X90-1 Proposal – Helicopter Instrument Flight Program Kellett

Feb 26 1958

55 Report No. 122V-90-1 Proposal-A Research Program for the Reduction of Helicopter Vibrations Kellett

Mar 15 1957

56 Report No. 1136 Charts for Determining the Aerodynamic Apr 1949

44

Characteristics of Jet Rotors in Hovering Contract AF 33 (038)-937, E.O. No. 582-164 McDonnell Aircraft

57 Report No. 1078 Charts for Estimating Blade Stall for Jet Rotors Contract# AF 33 (038)-937 McDonnell Aircraft

Mar 18 1949

58 Report No. 1079 Charts for Estimating the Autorotative Performance of Jet Rotors Contract# AF 33(038)-937 McDonnell Aircraft

Mar 18 1949

59 Report No. 248 A review of Rotor Induced Velocity Field Theory Contract# N6 onr-27015 Project NR 212-005

Jan 1954

60 AFFTC-TR-61-1 YHC-1A Flight Evaluation Feb 1961 61 AFFTC-TR-61-8 Limited Stability and Control Evaluation

of the S-62A Helicopter Mar 1961

62 Report No. 27-98-4 Report on Rotor Stability Contract# N­156s 26506 Prewitt

Apr 20 1949

63 CAL Report No. 75 A Two-Dimensional Approximation of the Unsteady Aerodynamics of Rotor wings Cornell

Oct 1955

64 Report No. AD-210 613 The Computed Instantaneous Velocities Induced at the Blade Axes by the Skewed Helical Vortices in the Wake of a Lifting Rotor in Forward Flight Contract# Nonr 991(05) Georgia Tech

Mar 1959

65 Report No. 15-A-15 Report on Methods and Computations Used in Selecting Rotor Physical Characteristics and Efficiencies Contract# W33-038 AC 21399 Piasecki

Aug 9 1949

66 Report No. 15-A-15 Appendix 14-A-03Report on Methods and Computations Used in Selecting Rotor Physical Characteristics and Efficiencies Contract# W33-038 AC 21399 Piasecki

Aug 9 1949

67 System Concepts and Research Aircraft Bell Helicopter Sep 1972 68 AFFDL-TR-69-34 Three-Axis (Self-Organizing) VTOL

Flight Control System for Comparing Rate, Attitude and Velocity Commands

Jun 1969

69 Letter from Piasecki Aircraft to Mr. B. Lindenbaum concerning Aquagyro

Jul 6 1961

70 Miscellaneous Unidentified Helicopter Photos (4) undated 71 Lockheed Rigid Rotor Report Vol. II, No. 2 Dec 1966 72 AHS Newsletter Vol. 5, No. 12 Dec 1959 73 HC-1B Category I Performance, Stability and Control

Flight Test Plan Mar 1962

74 Report No. R-294 Summary Presentation – USAF SR-175 VTOL/STOL Logistics Aircraft Parameter Study 1965­1970 Time Period

Apr 8 1960

75 Lockheed Reports Volume XI, Number 2 Mar 1962 76 WADD TR 61-66 A Study to Correlate Flight Measured

Helicopter Vibrations Data and Pilot Comments Boeing/Vertol

Aug 1961

77 AFM 60-19 H-19 Aircrew Standardization/Evaluation Feb 20 1962

45

Manual 78 Report No. ER 10281 ROTOPROP Interim Progress

Report Martin Jul 1958

79 AFV/F380-002 Proposal for the Development of a Helicopter Rotor Martin

Apr 16 1958

80 Trip Report – Purpose of Obtaining Information on Helicopters and Thrust Information

Mar 6-10 1950

81 AHS Newsletter Vol. 8, No. 3 Mar 1962 82 Report No. 533.5 A Proposal for the Study and Test of a

Lightweight Rotor System Hiller Apr 1956

83 Report No. 30-929-109 Response of Helicopter Rotors to Periodic Forces Bell

Oct 12 1944

84 Report No. 02-943-063 Periodic Aerodynamic Forces on Rotors in Forward Flight Bell

Feb 30 1944

85 AIAA Paper No. 71-991 The Reduction of VTOL Operational Noise Through Flight Trajectory Management

Oct 25-28 1971

86 Journal of Aircraft Volume 1 Number 6 Nov-Dec 1964 87 Journal of the Aeronautical Sciences Volume 11, No. 3 Jul 1944 88 Journal of the Aeronautical Sciences Volume 12, No. 1 Jan 1945 89 Journal of the Aeronautical Sciences Volume 13, No. 12 Dec 1946 90 Journal of the AHS Volume 5, No. 1 Jan 1960 91 Journal of the AHS Vol. 10, No. 3 Jul 1965 92 NASA Report 72-04 An Investigation of the Mixing of

Linear and Swirling Flows Contract# N00014-71-C-0226 Feb 15 1971 – Feb 14 1972

93 Report No. MDC-J56/01 Wind Tunnel Tests of Two Airfoils Designed for High Lift Without Separation in Incompressible Flow McDonnell Douglas

Aug 1972

94 Helicopter and V/STOL Noise Generation and Suppression Nov 1968 95 Sikorsky S-64 (Skycrane) Photos and Pictures 6 items 1960 96 ADS TN 68-1 A Study of the Army Hot Day Design

Hover Criterion Aug 1970

97 Bell Flyers Model 214A/B and YAH 63 May 1975 98 Boeing-Vertol Presentation to ASC, WPAFB Jul 26 1968 99 Rotary Wing Aircraft in the 1970-1980 Period Apr 14 1961 100 Results of XR-8 Rigid Rotor Studies Sep 20 1945 101 Vertol Helicopter Pamphlet Model 107 Helicopter Aug 4 1958 102 Piasecki Blueprint Model PH-29 Undated

ROTOR BLADES 20 1 Bell Helicopter Telescoping Rotor Blades – Article and 3

Photos May 5 1947

2 Variable Diameter Rotor Bell Helicopter – Article, Photos (2) and Diagrams Total 9 Items

1964-1968

3-4 Variable Diameter Rotor Study Contract# F33615-71C­1186

Est. 1970

5 Variable Diameter Rotor – Grumman, Sikorsky, Piasecki 1968

46

Miscellaneous Documents 6 SER-50709 Variable Diameter Rotor Study Interim TR

Contract# F33615-71-C-1186 Bell Mar 1971

7-8 USAAMRDL TR 73-32 Dymanic Model Wind Tunnel Tests of a Variable Diameter, Telescoping Blade Rotor System (Trac Rotor) Contract# DAAJ02-68-C-0074

Jul 1973

9 AFFDL-TR-70-70 Effect of Root Cutout on Hover Performance Sikorsky

Jun 1970

10­11

Report 50718 Variable Diameter Rotor Study Draft Final Report Contract# F33615-71-C-1186

Jul 9 1971

12 AFFDL-TR-70-170 Variable Diameter Rotor Study Sikorsky

Jan 1972

13 Report 243-X-3 Cost Proposal for Investigation of the Techniques for and the Problems of Designing Variable Diameter Rotors Having Large Ratios of Extended to Retract Span Contract# F33615-71-R-1068 Piasecki

Aug 31 1970

14 Report 243-X-2 Proposal for Investigation of the Techniques for and the Problems of Designing Variable Diameter Rotors Having Large Ratios of Extended to Retract Span Contract# F33615-71-R-1068 Piasecki

Aug 31 1970

15 Report P-09-622A Variable Diameter Rotor Proposal Contract# F33615-71-R-1068 Parsons Includes Cover Letter, Proposal and 4 diagrams

Aug 28 1970

16 Development of the Trac Variable Diameter Rotor Concept by Richard M. Segel Sikorsky

Feb 17-19 1969

ROTORS/BLADES 21 1 VTOL – Miscellaneous Concept Photos and Charts 1968-1970

2 Report 12153-FR1(R) Helicopter Application Studies of the Variable Deflection Thruster Jet Flap Contract# N00014-69-C-0267 NR-212-195/1-2-69 (Code 461) Honeywell, Inc

Nov 1970

3 AHS 29th Annual National Forum – The Application of Circulation Control Aerodynamics to a Helicopter Rotor Model by Joseph B. Wilkerson, Kenneth R. Reader and Drew W. Linck

May 1973

4 AHS 30th Annual National Forum – Hingeless Circulation Control Rotor Blade Design by P.H. Kesling and Jaap Schmidt Lockheed

May 1974

5 AHS Midwest Regional Symposium on Rotor Technology – Circulation Control Rotor Flight Demonstrator by David R. Barnes and George A. McCoubrey KAMAM and Douglas G. Kirkpatrick Naval Ship R&D Center

Aug 1976

6 AHS 35th Annual National Forum – The Circulation Control Rotor Flight Demonstrator Test Program by

May 1979

47

Joseph B. Wilkerson, David R. Barnes and Frank A. Gill KAMAN / Naval Ship R&D Center

7 Report 77-0034 Hover Evaluation of the Circulation Control High Speed Rotor by Kenneth R. Reader Naval Ship R&D Center

Jun 1977

8 Report 77-0076 Circulation Control – An Updated Bibliography of DTNSRDC Research and Selected Outside References

Sep 1977

9 Report 77-0084 An Assessment of Circulation Control Airfoil Development Naval Ship R&D Center

Aug 1977

10 The Effects of Dual Controls on the Performance of an Elastically Twisting Rotor Blade Contract# DAAJ02-67-C­0068

May 1970

11 SER-2600-24 Engineering Progress Report No. 24 Phase I of Development of Convertiplane (Model S-57) Contract# AF33(038)-28076

Jun 8 1953

12 Classification of Rotor Types (Stowed and Wing) Undated 13 SPB-AF9063-US Stowed Rotor V/STOL Program

Planning Proposal Sikorsky Mar 23 1964

14 LR-21283 A Summary of Stopped Rotor Research and Development at the Lockheed-California Co.

Jan 22 1968

15 Stowable Rotor System for Reusable Launch Vehicle Lockheed-California

Undated

16 Ryan Stoppable Rotor – Photos and Articles 1962-1964 17 Limit Cycle Torsional Motion of Helicopter Blades Due to

Stall by N.D. Ham MIT and M.I. Young Boeing-Vertol Aug 30 1965

18 Report 107-2 Theoretical Determination of Rotor Blade Harmonic Airloads by R.H. Miller MIT Contract# Now 62-0100-d

Aug 1964

19 Report 159A-90-1 TREC 60-43 Stability and Control Handbook for Helicopters Contract# DA 44-177-TC-599 Kellett

Aug 23 1961

20 Report R 242 Fundamentals of Helicopter Stability and Control Contract# Now60-0469-f Boeing-Vertol

Feb 1961

21 PB 121097 Rotary Wing Aircraft Handbook and History Volume 5 Weight and Balance Contract# W33-038 ac­21804 (20695)

1954

22 Light Helicopter Drag Chart 1950-1980 Undated 23 NASA MEMO 1-7-53L A Wind-Tunnel Investigation of

Rotor Behavior Under Extreme Operating Conditions with a Description of Blade Oscillations Attributed to Pitch-Lag Coupling

Nov 14 1958

24 NASA MEMO 1-23-59L Maximum Mean Lift Coefficient Characteristics at Low Tip Mach Numbers for a Hovering

Feb 1959

48

Helicopter Rotor Having an NACA 641A012 Airfoil Section

25 NASA MEMO 2-28-59L Comparison of Measured Flapwise Structural Bending Moments on a Teetering Rotor Blade with Results Calculated from the Measured Pressure Distribution

Feb 6 1959

26 NASA MEMO 4-15-59L Charts of the Induced Velocities Near a Lifting Rotor

Mar 26 1959

27 NASA MEMO 5-7-59L Flight Investigation of Effects of Transition, Landing Approaches, Partial-Power Vertical Descents, and Droop-Stop Pounding on the Bending and Torsional Moments Encountered by a Helicopter Rotor Blade

Apr 6 1959

28 Report 347-V-1002 (HTC-AD-64-8) Effects of Blade Stall on Helicopter Rotor Blade Bending and Torsional Loads Final Report Contract# Now-0422-c

May 1 1965

29 Torsional Oscillation of Helicopter Blades Due to Stall by Norman D. Ham MIT and Maurice I. Young Boeing

Jan-Jun 1966

30 Short Takeoff and Landing for the High Speed Aircraft by John K. Wimpress Boeing

Feb 1966

31 An Engineering Approximation for the Aerodynamic Loading of Helicopter Rotor Blades by M. I. Young Boeing-Vertol

Aug 30-Sep 3 1965

32 D210-10379-1 Boeing Vertol Division 1972 Independent Research and Development Program Weight Estimation for Helicopter Design Analysis

May 19-22 1958

33 SER-1775 Tow Tests of H-5 (S-51) Helicopter Contract# AF 33(038)-7878 Sikorsky

Oct 19 1950

34 AHS 5th Annual Western Forum A Study of the Attainable Range of Helicopters by Abraham C. Adler and Helen S. Holm

Sep 25-26 1958

35 Report HTC-AD-65-15 Volume I Summary TR Rotor/Wing Concept Study Contract# Nonr-4588(00) Hughes Tool

Sep 1965

36 Report 7376 Substantiating Data on the Unloaded Rotor V/STOL Transport Aircraft McDonnell Aircraft

Feb 1 1960

37 NASA TN D-3028 Analytical Investigation of a Helicopter Rotor Driven and Controlled by a Jet Flap

Sep 1965

38 Technical Note AL-290 Design and Performance of a Prototype Circulation Control Helicopter Rotor

Mar 1973

39 High Advance Ratio Research and Development Lockheed-California

Feb 1970

40 Composite Aircraft with Rotary and Fixed Wing Components by Dr. J.A.J. Bennett Hiller

1952

41 Performance Characteristics of a Jet-Flap Rotor by John L. McCloud III, William T. Evans and James C. Biggers

Apr 4-5 1966

49

Ames Research Center 42 AHS 54th Annual Forum Compound Interest-A Dividend

for the Future, Revised by D.V. Humpherson Westland Helicopters

May 20-22 1998

43 AHS 54th Annual Forum A Perspective of Future Rotorcraft Technology by P.N. Goddard Westland helicopters

May 20-22 1998

44 Analytical Investigation of the Performance of a Controllable Twist Rotor Contract# DAAJ02-67-C-0068 KAMAN (3 copies)

Undated

45 Report 68-9 Reverse-Velocity Rotor Test Program Fairchild Hiller

May 29 1968

46 SPB 73-A6461-RD Full Scale Wind Tunnel Test of TRAC Sikorsky

Dec 17 1973

47 The Controllable Twist Rotor by Arthur F. Smith KAMAN

Jun 18-20, 1969

48 NASA TN D-2628 Wind Tunnel Investigation of a Lifting Rotor Operating at Tip-Speed Ratios from 0.65 to 1.45

Feb, 1965

49 Report 68-5 Reverse Velocity Rotor Model Wind Tunnel Test Program Results Fairchild Hiller

Jul 5 1968

50 Research and Development of Advanced Rotorcraft Concepts by Evan A. Fradenburgh Sikorsky

1968

51 DOD/NASA Aeronautical Research and Development Studt Rotorcraft Technology

Nov 1972

52 Development of the TRAC Variable Diameter Rotor Concept by Richard M. Segel and Evan A. Fradenburgh Sikorsky

Feb 17-19 1969

53 AHS 28th Annual National Forum The Controllable Twist Rotor, Performance and Blade Dynamics by A.Z. Lemnios and A.F.Smith KAMAN

May 1972

54 AHS 28th Annual National Forum Design Considerations of Circulation Control Rotors by Robert M. Williams and Ernest O. Rogers Naval Ship R&D Center

May 1972

55 Preliminary Investigation of the Karman-Yuan Helicopter Rotor System by S. W. Yuan Contract# AF 33(616)-2087

Undated

56 Technical Note AL-189 Theoretical Performance of a Pure Jet Flap Rotor at High Advance Ratios

Dec 1970

57 The Controllable Twist Rotor Pamphlet KAMAN Undated 58 Miscellaneous Photos (1) Fairey Rotodyne ; (2-3)

Advanced Blade Concept (ABC) Demonstrator Undated

1980 Propeller Propulsion Conference 22 1 Material -1)Cover Page; 2) Bookmark; 3) Sep 29 1982

Cover Letter Apr 22-24 1980

50

2 Lindenbaum Presentation Slides – Part 1 Apr 22-24 1980 3 Neitzel Presentation Slides Apr 22-24 1980 4 Foss Presentation Slides Apr 22-24 1980 5 Scherrer Presentation Slides Apr 22-24 1980 6 Pinson Presentation Slides Apr 22-24 1980 7 Redmond Presentation Slides Apr 22-24 1980 8 Scolatti Presentation Slides Apr 22-24 1980 9 Goldsmith Presentation Slides Apr 22-24 1980 10 Marks Presentation Slides Apr 22-24 1980 11 Slivinsky Presentation Slides Apr 22-24 1980 12 Nored Presentation Slides Apr 22-24 1980 13 Gatzer Presentation Slides Apr 22-24 1980 14 Lyon Presentation Slides Apr 22-24 1980 15 Correspondence Apr 22-24 1980 16 Miscellaneous Apr 22-24 1980 17 Planning Documents Apr 22-24 1980 18 Supporting Document – SAE 760535 Fuel Conservative

Propulsion Concepts for Future Air Transports by D.E. Gray & J.W. Witherspoon Pratt & Whitney

May 18-20 1976

19 Supporting Document- AIAA Paper No. 75-1208 – The Prop-Fan – A New Look in Propulsors by C. Rohrback & F.B. Metzger Hamilton-Standard

Sep 29-Oct 1 1975

20 Supporting Document- AIAA Paper No. 76-667 A Report on the Aerodynamic Design and Wind Tunnel Test of a Prop-Fan Model by Carl Rohrbach Hamilton-Standard

Jul 26-29 1976

21 Supporting Document- ASME 78-GT-201 Evolution of the Turboprop for High Speed Air Transport by G.E. Holbrook Detroit Deisel & G. Rosen Hamilton-Standard

Apr 9-13 1978

22 Supporting Document- SAE 751085 General Characteristics of Fuel Conservative Prop-Fan Propulsion System by B.S. Gatzen Hamilton-Standard & S.M. Hudson Detroit Diesel

Nov 17-20 1975

23 Supporting Document- AGARD Multi-Mission Uses for Prop-Fan Propulsion by A.H. Jackson, Jr. & B.S. Gatzen Hamilton-Standard

Sep 1976

24 Supporting Document- SAE 771009 Advanced Turboprop Propulsion Reliability and Maintenance Costs by Philip C. Stolp Detroit Diesel & James A. Baum Hamilton-Standard

Nov 14-17 1977

25 Supporting Document- AIAA Paper No. 79-1116 Structural Design and Analysis of Prop-Fan Blades by R.W. Cornell & E.A. Rothman Hamilton-Standard

Jun 18-20 1979

26 Supporting Document- SAE 780995 Prop-Fan Propulsion – Its Status and Potential by James F. Dugan, Jr. NASA & Bernard S. Gatzen and William M. Adamson United Technologies

Nov 27-30 1978

27 Supporting Document- AIAA Paper No. 79-0610 Mar 12-14 1979

51

Aeroacoustic Design of the Prop-Fan by F.B. Metzger & C. Rohrbach Hamilton-Standard

28 Supporting Document- B202 Rev A Propeller Progress Hamilton-Standard

Mar 1968

29 Supporting Document- AIAA Article – A Design Perspective on New Technologies for General Aviation by “JB” McCollough FAA

1979

30 Supporting Document- AWST Prop-Fan Powerplant Studies Evolve by Warren C. Wetmore

Jan 3 1977

31 Supporting Document- A fan for Tomorrow by Gene Costello Hamilton-Standard

1978

32 Proceedings of the 1980 Conference on Propeller Propulsion

Apr 22-24 1980

33 Supporting Document- Hamilton Standard Prop-Fan Data Packages

Feb 28 1978

34 Supporting Document- SP 11A77 Prop-Fan Fuel Conservative Propulsion for the 1980’s High Speed Air Transports Hamilton Standard

Oct 1977

35 Supporting Document- SP 07A77 Prop-Fan Technology Status Report

Undated

36 Supporting Document- SP 02A77 Prop-Fan Fuel Conservative Propulsion for the 1980’s High Speed Air Transports Hamilton Standard

Jan 1977

37 Report on Apr 22-24 1980 Propeller Propulsion Conference and Subsequent Activities

Undated

38 Supporting Document- Potential Propeller Technology and Static Thrust Augmentation by George Rosen Hamilton Standard

May 17 1966

39 Supporting Document- Glass Fiber Reinforced Plastic Blades for VTOL/VSTOL Aircraft Propellers Curtiss-Wright

1961

40 Supporting Document- All-Mechanical Propeller Curtiss-Wright

Dec 1958

41 Supporting Document- SP 06A77 Prop-Fan Acoustics – Status Hamilton Standard

Apr 1977

42 Supporting Document- Proposed Propeller Development for High Speed STOL and V/STOL Aircraft

Feb 14 1968

43 Miscellaneous AWST Articles and Advertisements Various 44 Attendees Names and Addresses 45 Support Letters from Industry Various 46 Correspondence Various 47 Technical Correspondence Various 48 Miscellaneous Presentation Pages Undated 49 Supporting Document- EDR10280 A Presentation on

Reduction Gearing by Terry Lyon Detroit Diesel Apr 21 1980

50 Presentation- Review of Propeller Propulsion Progress Up Undated

52

to the 1970s by Charles Scolatti 51 Supporting Document- Review of Propeller Propulsion

Progress Up to the 1970s A Success Story by Charles Scolatti

Undated

52 Marks Presentation Undated 53 Goldsmith Presentation Undated 54 Supporting Document- Soviet TU-95, TU-114 and AN-32

Aircraft Undated

55 Supporting Document- Blueprint of Prop-Fan on C-141A Mar 18 1980 56 Advanced Prop-Fan Engine Technology (APET)

Definition Study – Task II Review Contract# NAS3-23044 GE

Aug 5 1982

57 NASA CR159355 Turboprop Cargo Aircraft Systems Study Phase I Contract#NAS1-15708

Nov 1980

58 Miscellaneous Notes and Contact Lists Undated 59 Prop-Fan Propulsion Briefing Charts Undated 60 Scherrer Presentation Undated 61 Supporting Document- Commuter Traffic Statistics – New

Horizons 1978

62 Miscellaneous Photos Undated

ROTOR/BLADE TESTS & HELO CONTROL 23 1 NACA TN 1245 Summary of Lateral-Control Research Mar 1947

2 NACA TN 2474 Empirical Relation Between Induced Velocity, Thrust, and Rate of Descent of a Helicopter Rotor as Determined by Wind-Tunnel Tests on Four Model Rotors

Oct 1951

3 UH2C Pamphlet KAMAN Undated 4 Flight Test of the FRG 32-301 Hover/Transition and

Aerodynamic Damper/EFS – Integrated Fly by Wire SAS 1969

5 Report FT23-4R-64 Final Report Military Research Evaluation of the Lockheed XH-51A Rigid Rotor Helicopter

Jan 7 1964

6 AHS 27th Annual National V/STOL Forum – Forward Flight Performance of a Coaxial Rigid Rotor by Vincent M. Paglino Sikorsky

May 1971

7 ONR Conference VTO-Cargo Aircraft – Letters and Notes Oct 24-25 1955 8 The Driven Rotor Model Design – Sketches Jul 12 1982 9 WADC TR 57-583 – Part I – Helicopter Configuration and

Propulsion Systems Study Part I Statistical Weight Analysis Contract# AF33(616)-3149

Nov 1957

10 WADC TR 57-583 – Part III – Helicopter Configuration and Propulsion Systems Study Part III Aerodynamic Analysis Contract# AF33(616)-3149

Nov 1957

11 WADC TR 57-583 – Part IV – Helicopter Configuration and Propulsion Systems Study Part IV Analytical

Nov 1957

53

Procedure for Predicting Rotor Weight Contract# AF33(616)-3149

12 NASA TN D-809 Tables and Charts of the Normal Component of Induced Velocity in the Lateral Plane of a Rotor with Harmonic Azimuthwise Vorticity Distribution

Apr 1961

13 NASA Memo 3-3-59L Wind-Tunnel Investigation of the Effect of Angle of Attack and Flapping –Hinge Offset on Periodic Bending Moments and Flapping of a Small Rotor

Mar 1959

14 Report F-TS-1045-RE The Power Required of the Ideal Helicopter (from German)

Jan 1947

15 Report F-TS-510-RE Air and Mass Forces on Helicopter Propellers with Inclined Hinge (from German)

Mar 30 1946

16 Report F-TS-616-RE The Sensitiveness of the Human Body to Vibrations (from German)

Sep 1946

17 Report F-TS-692-RE The Pull-Up of the Helicopter (from German)

Aug 1946

18 Report F-TS-1001-RE The Performance Characteristics of the Helicopter (from German)

Sep 1946

19 Report F-TS-1002-RE The Dynamic Stability of Helicopters with Articulated Rotors(from German)

Sep 1946

20 Report F-TS-1003-RE Static Thrust Tests of the Model Helicopter Rotor and Preliminary Research of the Model Helicopter Rotor (from German)

Sep 1946

21 Report F-TS-1004-RE The Theory of the Control of the Blade Angle of the Helicopter (from German)

Sep 1946

22 Report F-TS-1006-RE Theory of Helicopter Control in Hovering Flight (from German)

Sep 1946

23 Report F-TS-1007-RE Investigation of the Influence of High Subsonic Velocities on the L/D of Rotary Wing Aircraft (from German)

Sep 1946

24 Report F-IR-133-RE Helicopter Theory Interview with Dr. Kurt Hohenemser Concerning His Recent Contributions

Sep 1946

25 NACA TM 907 Dynamic Stability of a Helicopter with Hinged Rotor Blades

Sep 1939

26 AF TR No. 6352 Longitudinal Stability Characteristics of a Gyroscopically Stabilized Helicopter in Forward Flight

Mar 1951

27 NACA TN 2721 Initial Results of Instrument- Flying Trials Conducted in a Single-Rotor Helicopter

Jun 1952

28 NACA TN 1430 A Theoretical Study of the Dynamic Properties of Helicopter-Blade Systems

Nov 1948

29 NACA TN 1999 A Theoretical Analysis of Elastic Vibrations of Fixed-Ended and Hinged Helicopter Blades in Hovering and Vertical Flight

Jan 1950

30 NACA TN 2984 Studies of the Lateral-Directional Flying Qualities of a Tandem Helicopter in Forward Flight

Aug 1953

31 NACA TN 3089 One-Dimensional, Compressible, Viscous Dec 1953

54

Flow Relations Applicable to Flow in a Ducted Helicopter Blade

32 NACA TN 3201 Directional Stability Characteristics of Two Types of Tandem Helicopter Fuselage Models

May 1954

33 USAAVLABS TR 68-22B In-Flight Measurement and Correlation with Theory of Blade Airloads and Responses on the XH-51A Compound Helicopter Rotor Volume II Measurement and Data Reduction of Airloads and Structural Loads Appendixes V through IX Contract# DA 44-177-AMC-357(T)

May 1968

34 ER Number 63-26 Preliminary Design Study Notes – Proposal for a Ground Test Research Program –Tip Turbojet Powered Heavy-Lift Rotor System Hiller

1962-1963

35 Project Forecast – High Speed Flexure Hub Rigid Rotor System for Helicopters Lockheed-California

Undated

36 AHS West Coast Forum Application of System Analysis Methods to Helicopter Preliminary Design by John A. DeTore & Eugene L. Brown

Nov 4-6 1954

37 Progress Report for NACA Helicopter Subcommittee Meeting

Apr 16 1958

38 AFFTC-TR-60-2 Air Force Flight Evaluation YHO-2HU Feb 1960 39 NACA TN 2912 The Normal Component of the Induced

Velocity in the Vicinity of a Lifting Rotor and Some Examples of its Application

Mar 1953

40 The Djinn Helicopter Cold Cycle Tip Jet YHO-1DJ Pamphlet Republic

Undated

41 Report No. 362 Stability ond Control of Tandem Helicopters Phase I and II – Static and Dynamic Longitudinal Stability and Control Princeton University

Sep 1956

42 Report XX90-4 Proposal for a Theoretical and Experimental Study of a Helicopter Employing Fixed Wings and Cocked Flapping and Lag Blade Hinges Kellett

Mar 1954

43 NACA TN 2086 Hovering and Low-Speed Performance and Control Characteristics of an Aerodynamic-Servocontrolled Helicopter Rotor System as Determined on the Langley Helicopter Tower

May 1950

44 NACA TN 2154 An Analysis of the Autorotative Performance of a Helicopter Powered by Rotor-Tip Jet Units

Jul 1950

45 NACA TN 3900 Investigation of Vertical Drag and Periodic Airloads Acting on Flat Panels in a Rotor Slipstream

Dec 1956

46 NACA TN 1595 Analysis of Flight-Performance Measurements on a Twisted, Plywood-Covered Helicopter Rotor in Various Flight Conditions

Jun 1948

55

47 NACA TN 3234 Reduction of Helicopter Parasite Drag Jun 1954 48 NACA Helicopter Subcommittee Meeting – Helicopter

Stabilizer with Photo Oct 22 1948

49 Prediction of Helicopter Longitudinal Stability and Control Characteristics – A Comparison Between Flight Test and Theory by Edwin R. Schultz (Master’s Thesis)

May 1958

50 WADC TR 55-437 Part I An Investigation of the Handling Qualities of a Sikorsky H-19 Helicopter Equipped with Various Mechanical Stabilizers Part I-Analytical Evaluation of Stabilizers Contract# AF33(616)-2780

May 1957

51 Bell Model 47-J Four Place Multi-Purpose Helicopter Pamphlet

Undated

52 Report FTR 47-2 Skid Landing Gear – Effect on Model 47 Bell

Sep 9 1952

53 Report X-417-11A XR-8 Model Specification Kellett May 3 1945 54 Report FTM 47-6 Drag Analysis of H-13E and Proposed

Configurations Bell Feb 4 1953

55 Report No. 120.30 Specification for Model XR-10 Helicopter Kellett

Mar 21 1944

56 Notes on Visits in Europe by Grover Loening with Photos Ovt 1952 57 NASA TN D-73 Comparison of Calculated and Measured

Stall Boundaries of a Helicopter Rotor at Advance Ratios from 0.3 to 0.4

Sep 1959

58 NASA TN D-393 Measurements of the Time-Averaged and Instantaneous Induced Velocities in the Wake of a Helicopter Rotor Hovering at High Tip Speeds

Jul 1960

59 NASA TN D-112 Experimental Investigation of the Pressure Fluctuations on a Flat Plate and a Cylinder in the Slipstream of a Hovering Rotor

Sep 1959

60 NASA TN D-737 Some Recent Studies in Structural Dynamics of Rotor Aircraft

Mar 1961

61 NASA TN D-742 Hovering Characteristics of a Rotor having an Airfoil Section Designed for Flying-Crane Type of Helicopter

Apr 1961

62 NASA TN D-774 Operational Technique for Transition of Several Types of V/STOL Aircraft

Mar 1961

63 NASA TT F-43 A Vibration Absorber for Two-Bladed Helicopters (from French)

Nov 1960

64 NASA TT F-55 Response of a Helicopter Rotor to an Increase in Collective Pitch for the Case of Vertical Flight (from French)

Jan 1961

65 NASA CR-2009 A Method for Analyzing Dynamic Stall of Helicopter Rotor Blades

May 1972

66 US Army TRC Preliminary Flight Test Data – Xh-51A Nov 1964

56

Rigid Rotor High Speed Flight Program 67 Performance Substantiation for Kinedyne Proposal Cessna Feb 5 1958 68 WADC TR 55-437 Part II An Investigation of the

Handling Qualities of a Sikorsky H-19 Helicopter Equipped with Various Mechanical Stabilizers Part II-Flight Test Evaluation of the Optimum Stabilization System Contract# AF33(616)-2780

Jan 1958

69 R. & M. No. 1730 The Flight of a Helicopter by H.B. Squire, M.A. (British Air Ministry)

Nov 28 1935

70 NASA TN D-335 Full-Scale Wind-Tunnel Tests of Blowing Boundary-Layer Control Applied to a Helicopter Rotor

Sep 1960

71 NASA TN D-432 A Summary of Operating Conditions Experienced by Three Military Helicopters and a Mountain-Based Commercial Helicopter

Oct 1960

72 NASA TN D-464 Effects of Control-Response Characteristics on the Capability of a Helicopter for use as a Gun Platform

Sep 1960

73 NASA TN D-534 Hovering Measurements for Twin-Rotor Configurations with and without Overlap

Nov 1960

74 NASA TN D-537 Flight Evaluation of Several Spring Force Gradients and a Bobweight in the Cyclic-Power-Control System of a Light Helicopter

Oct 1960

75 R. & M. No. 885 Some Experiments on Airscrews at Zero Torque, with Applications to a Helicopter Decending with the Engine “Off”, and to the Design of Windmills by C.N.H. Lock, M.A. & H. Bateman, B.Sc. (British Air Ministry)

Sep 1923

76 Technical Note WCT-52-47 Functional Development Test of the YH-24SE Helicopter

Dec 1952

77 WADC TR 55-438 Part I The Determination of Helicopter Longitudinal Stability Derivatives from Flight Test Data Part I. Development of Flight Test Instrumentation, Techniques and Analysis Methods Contract# AF33(616)­2773

Feb 1958

HELICOPTER AND BLADE AERODYNAMICS 24 1 Report SB-862-S-4 Investigation of Helicopter Rotor

Flutter and Load Amplification Problems Contract# AF 33(616)-440 Cornell

Aug 1956

2 Report No. 299-099-072 Proposal for the Construction and test of an Experimental Rotor Blade Suitable for Operation at High Tip Mach Number Bell

Nov 6 1957

3 NACA TN 3323 Charts for Estimating Performance of High-Performance Helicopters

Oct 1954

4 US Naval Air Test Center Model HRS-1, BuNo 127824 Mar 24 1954

57

Flight Test and Evaluation of JATO Installation Final Report

5 DADC Helicopter Rotor Testing Facilities Propeller Laboratory Design Features

Jun 24 1955

6 Report AVN 1556 Service Test of the HOK-1 Helicopter Mar 1957 7 Report UTR No. 150.1 The Helicopter Control Rotor

United Helicopters, Inc. Mar 19 1947

8 The “SKEETER” Mark 6 Helicopter Sanders-Roe Limited C.A. 1949 9 Report No. G-113-6 Flutter Analysis of the KAMAN K­

16B VTOL/STOL Research Aircraft Contract# NOa(s) 56­549c

Oct 15 1959

10 Report No. 269-S-1 Final Design Specification for Hughes Tool Company – Aircraft Division Two-Place, Single Engine, Three Bladed Helicopter Model 269A

Jun 5 1957 Rev1 Jul 1 1957

11 US Naval Air Test Center Evaluation of Stability and Control Characteristics of Model HRP-1 Helicopter BuNo 111809 with Stabilizer Device

Dec 26 1950

12 Report No. 230 Model Study of Helicopter Dynamic Stability and Control Phase II Comparison of Theoretical and Experimental Results Near Hovering Flight Princeton University

May 1953

13 Report 204-099-903 Structural Comparison of Six Multi-Bladed Rotor Designs Contract# AF 33(600)30229 Bell

Apr 12 1957

14 Report 204-099-907 Evaluation of Five Semi-Rigid Multi-Blades Rotor Designs Contract# AF33(600)30229 Bell

Jul 25 1957

15 Report 204-099-701 The Dynamics of Semi-Rigid Multi-Blade Rotors Contract # 33(600)30229 Bell

Sep 3 1957

16 Report 204-099-706 Preliminary Studies on the Design of Blades for Semi-Rigid Rotors to Minimize Vertical Vibration Contract# 33(600)30229 Bell

Sep 3 1957

17 Report SER-383 Mechanical Instability Characteristics of the H-5G Helicopter Contract# AF 33(038)-2662

Apr 15 1949

18 American Helicopter Co. XA-6 and H26 Helicopter Brochures

Undated

19 Report No. 123-G1 Performance Analysis XA-5 Pulse Jet Powered helicopter Contract# AF 33(038)-6099 AHC.

May 1 1950 Rev May 26 1950

20 Summary Report 123-O-1 Pulse-Jet Engine Development Contract# AF 33(038)-6099 AHC

Sep 14 1950

21 Summary Report 123-O-2 Development of Pulse-Jet Helicopter Rotor Contract# AF 33(038)-6099 AHC

Sep 14 1950

22 Report 123-B1 Pulse Jet Rotor design Analysis Contract# AF 33(038)-6099 AHC

Oct 5 1949

23 Report 163-B-2 Altitude Performance and Operational Tests of Pulse-Jet Engines AHC

Dec 20 1950

58

24 Report 157-1 Model 157 Single-Place Pulse-Jet Propelled helicopter (Collapsible) AHC

Feb 22 1951

25 Report 157-3 Aerodynamics Analysis of a Single-Place, Jet-Propelled Helicopter Model 157 AHC

Feb 22 1951

26 Report 163-F-1 Analysis of the Dynamic Forces in the Control System of the XA-5 Pulse-Jet-Powered Helicopter 25 Report 157-3 Contract# AF 033(038)-6099 AHC

Apr 6 1951

27 Report 157-b Model Specification Model 157, Single Place Helicopter AHC

Jun 8 1951

28 Report 163-H-1 A Mathematical Analysis of the Response Characteristics of a Two-Bladed, Jet-Driven Rotor to Vertical Excitation Helicopter Contract# AF 033(038)­6099 AHC

Jun 21 1951

29 Report 163-L Progress Report for Sep 1951 – Development of a Pulse-Jet-Powered Helicopter Rotor Contract# AF 33(038)-6099 AHC

Oct 20 1951

30 Report 163-I Progress Report for Jun 1951 – Development of a Pulse-Jet-Powered Helicopter Rotor Contract# AF 33(038)-6099 AHC

Jul 14 1951

31 XH-26 Single Place Helicopter (Collapsible) Mock Up Board Information AHC

1951

32 Report S-157-k Proposed Model Specification, Model XH­26A Two-Place, Observation-Reconnaissance-Utility Helicopter Contract AF 33(038)-27961 AHC

Oct 31 1952

33 American Helicopter Co. Progress Notes Feb 8 1954 34 Report No. TCAR001 Model Specifications Model TCAH­

1 Twin Coach Jun 9 1953

35 Report No. TCAR002 Preliminary Performance of the Twin Coach Model No. TCAH-1 Helicopter Twin Coach

Aug 19 1953

36 Report No. S-157-Q ERs Model XH-26 Contract# AF 33(038)-27961 ( 13 separate reports)

1953

37 Report No. S-157-C ERs Model XH-26 Contract# AF 33(600)-5860 ( 10 separate reports)

1953

38 Report No. S-157-EE ERs Model XH-26 Pulse-Jet Helicopter Contract# AF 33(038)-27961 ( 6 separate reports)

1953

HELICOPTER PERFORMANCE & THEORY 25 1 Report No. 48-923-001 Preliminary Flight Test of XR-12

Helicopter Bell Apr 28 1948

2 NASA TN D-1364 A Wind Tunnel Investigation of the Longitudinal Aerodynamic Characteristics of Two Full-Scale Helicopter Fuselage Models with Appendages

Jul 1962

3 Technical Note WCT-53-16 Cornell Rotor Stabilizer Mar 1953 4 Experimental Study of a Tandem Helicopter Employing

Cocked Vertical Blade Hinges Kellett Jan 25 1956

59

5 NASA TN D-1363 A Wind Tunnel Investigation of the Drag and Static Stability Characteristics of Four Helicopter Fuselage Models

Jul 1962

6 Report Number 62-73 Proposal to USAF for use of Model Ten99A as a Missile Site Support Helicopter Hiller

Aug 1962

7 FTC-TDR-62-15 Performance Evaluation of the H-13K Aug 1962 8 Report No. 373 An Economical Technique for the

Construction and Hovering Flight Evaluation of Dynamically Similar Helicopter Models Princeton

Nov 1956

9 Report No. F-IR-133-RE Helicopter Theory Interview with Dr. Kurt Hohenemser

Sep 1946

10 Report No. F-IR-1001-RE The Performance Characteristics of the Helicopter by Dr. Kurt Hohenemser

Sep 1946

11 Report No. 30-929-113 Stability of Helicopter Having Universal Joint Two Blade Rotor Bell

Nov 26 1942

12 SER-442 The Effect of Platform on Static Thrust Performance Sikorsky

Nov 7 1944

13 SER-459 Tilted Tail Rotor Aerodynamic Study of New tail Arrangement Sikorsky

Feb 7 1945

14 SER-3104 Substantiating Data for Standard Aircraft Characteristics and Performance Charts for H-34A Helicopter Sikorsky

Aug 16 1954 RevA Mar 15 1955

15 Report F-TS-5406-RE The Danger of the Side Drift Landing in the Operation of Rotary Wing Aircraft by S. Hoerner (Germany)

Apr 1948

16 Report F-TS-1045-RE The Power Required for the Ideal Helicopter by K. Hohenemser (Germany)

Jan 1947

17 Report No. 156 An Experimental Investigation of the Transition of a Helicopter from Hovering to Vertical Flight Contract# NAw-5619 Princeton University

Dec 1 1949

18 AHS Design Considerations in the Kaman Servo-Controlled Intermeshing-Rotor Helicopter by Charles H. Kaman

Feb 9 1953

19 Progress Report – Unsteady Induced Flow on Helicopter Rotors Contract# NAw-5619 Princeton

Jun 1 1949

20 Report No. AA-1-6 Loading Analysis Theory for a Four-Bladed Universally Mounted Rotor System Contract# AF33(600)-9053

Sep 30 1953

21 Proposed Rotorcraft Design, Inherently Stable in Pitch and Roll, with a Simplified Control System by J.C.Vogtle & H. E. Stewart

Nov 28 1953

22 Flight Testing Helicopters for Dynamic Stability (Cornell Aero Lab Utilizing YH-13 Helicopter) by John O’Dea

Undated

23 Report AD No. 16-727 Design and Development of an Automatic Hovering Control for Rotary Wing Aircraft

May 15 1953

60

Final Report Number 111 – Phase I Contract# AF 33(616)­227

24 Report No. R50GL174 Biased Cyclic Control for H-5 Helicopter Contract# AF33(083)6146

Jun 1 1950

25 Report No. 58-19 Damped Bar Stabilized Control Rotor System Hiller Helicopters

Jan 6 1958

26 Report GER-3005 (Photocopy) Theoretical Stability and Control Study for H-5 Helicopter Goodyear

Feb 1949

27 Report EP-247-0958-12 Proposal for Flight Test and Evaluation of Hydromechanical Stability Augmentation System Vertol t

Sep 22 1958

28 Report 1430.17 An Approximate Analysis of the Static Longitudinal Stability of a Tandem-Type Helicopter, with Applications to Kellett Model KH-3 Skycrane Kellett

Jan 1946

29 Report PTR AD-3096 Navy Evaluation of the Modified Model HSL-1 Helicopter, Report No. 1, Final Report

Jan 15 1960

30 Report YA-1533 Stability and Control Analysis of the M­30 Quadrotor Transport Helicopter Convertawings

Jul 9 1958

31 File No. 565-PH-56-91(5004) Final Report on Study of Helicopter Stabilization Systems Contract# DA-36-039 SC-72412

Jun 1 1956 to 31 Jul 1957

32 AFFTC-TR-58-4 ARDC H-19 Stability with a Stabilizing Bar

Mar 1958

33 AHS 30th Annual National Forum – Doc# 800 – Laser Velocimeter measurements of the Helicopter Rotor-Induced Flow Field by James C. Biggers & Kenneth L. Orloff Ames research

May 1974

34 AHS 30th Annual National Forum – Doc# 801- The Prediction of Rotor Rotational Noise Using Measured Fluctuating Blade Loads by R.N. Hosier, R. Ramakrishnan & R.J. Pegg NASA Langley

May 1974

35 AHS 30th Annual National Forum – Doc# 802- Tail-Rotor Thrust on a 5.5-Foot Helicopter Model in Ground Effect by R. Wayne Empey & Robert A. Ormison Ames Directorate, Moffitt Field

May 1974

36 AHS 30th Annual National Forum – Doc# 803- Can Helicopter Rotors be Designed for Low Noise and High Performance? By David R. Clark Sikorsky

May 1974

37 AHS 30th Annual National Forum – Doc# 804- A Systematic Study of Helicopter Rotor Stall Using Model Rotors by Anton J. Landgrebe & E. Dean Bellinger United Aircraft

May 1974

38 AHS 30th Annual National Forum – Doc# 810- Design to Cost at Work for Helicopter Systems by Leonard J. Marchinski Boeing Vertol

May 1974

61

39 AHS 30th Annual National Forum – Doc# 811- Improved Cost Effectiveness of Helicopters Through a Two-Point Design Criterion by Arved Plaks & Richard C. Meier Kaman and Herman I. MacDonald USAAMRDL

May 1974

40 AHS 30th Annual National Forum – Doc# 812- The Scissors Rotor by Walter G.O. Sonneborn & Jan M. Drees Bell Helicopter

May 1974

41 AHS 30th Annual National Forum – Doc# 821- Visual and Manual Workload of the Helicopter Pilot by Dr. Dora Dougherty Strother Bell Helicopter

May 1974

42 AHS 30th Annual National Forum – Doc# 822- Helicopter Command Instrument Systems by James F. Hatcher US Army ASC

May 1974

43 AHS 30th Annual National Forum – Doc# 824- Avionic and Fire Control Equipment Complement to Enhance Attack Helicopter Survivability by Edward Stepans Lockheed-California

May 1974

44 AHS 30th Annual National Forum – Doc# 825- Controls and Displays for Helicopter IFR Operation – Pilot Factor Considerations by F.J. Winter, Jr. WPAFB Flight Dynamics Lab

May 1974

45 AHS 30th Annual National Forum – Doc# 831- On the Use of First Order Rotor Dynamics in Multiblade Coordinates by K.H. Hohenemser & S.K. Yin Washington Univ (St.Louis)

May 1974

46 AHS 30th Annual National Forum – Doc# 832- Effect of Hub Impedence on the Inplane Oscillatory Blade Loads of a Two-Bladed Rotor System by J.A. White & C.D. Lee Bell

May 1974

47 AHS 30th Annual National Forum – Doc# 833- Effect of Blade Design Parameters on Helicopter Stall by R.H. Blackwell Sikorsky & P.H. Mirick USAAMRDL

May 1974

48 AHS 30th Annual National Forum – Doc# 834- AH-56A (AMCS) Compound Helicopter Vibration Reduction by W.D. Anderson & E.R. Wood Lockheed-California

May 1974

49 AHS 30th Annual National Forum – Doc# 842- Rotor Moment Control with Flap-Moment Feedback by A.J. Potthast & A.W. Kerr Lockheed-California

May 1974

50 AHS 30th Annual National Forum – Doc# 843- Analysis, Simulation, and Piloted Performance of Advanced Tandem-Rotor Helicopters in Hover by Robert P. Smith USAAMRDL & Roman T. Lytwyn & F. White Boeing Vertol

May 1974

51 AHS 30th Annual National Forum – Doc# 844- Helicopter Icing Handling Qualities by LTC Warren E. Griffith II &

May 1974

62

CPT Larry K. Brewer US Army Avn Systems Test Activity (Edwards AFB)

52 AHS 30th Annual National Forum – Doc# 850- Fabrication of Boron-Hybrid Swashplates by Joseph Jakubowski & Alexander Yankovoy Boeing Vertol

May 1974

53 AHS 30th Annual National Forum – Doc# 852- Heat Transfer Modeling for Curing Process of Composite Rotor Blades by Tai Lang Huang & Andrew A. Peterson Boeing Vertol

May 1974

54 AHS 30th Annual National Forum – Doc# 853- Processing of Titanium Tubes – An Approach to Helicopter Blade Spar Manufacturing by Stanley M. Silverstein Sikorsky

May 1974

55 AHS 30th Annual National Forum – Doc# 860- Helicopter Reliability Testing by Thomas L. House USAAMRDL

May 1974

56 AHS 30th Annual National Forum – Doc# 861- RAPID – A Data Acquisition and Processing System for Flight Test Cost and Schedule Improvement by Victor G. Berecz Sikorsky

May 1974

57 AHS 30th Annual National Forum – Doc# 862- Helicopter Flight Investigation to Determine the Effects of a Closed-Circuit TV on Performance of a Precision Sling-Load Handling Task by Danial J. DiCarlo NASA Langley, Henry L. Kelley USAAMRDL & David L. Spivey CWO, US Army

May 1974

58 AHS 30th Annual National Forum – Doc# 863- Effect of Nap-Of-The-Earth Requirements on Aircrew Performance During Night Attack Helicopter Operations by COL Billy L. Odneal US Army Comcat Developments Experimentation Cmd.

May 1974

59 AHS 30th Annual National Forum – Doc# 864- UTTAS Flight Test: Real-Time Data Analysis by Donald L. Marshall & Herbert H. Steinmann Boeing Vertol

May 1974

60 AHS 30th Annual National Forum – Doc# 870- Heavy-Lift Helicopter Engine Control System by J. Roger Alwang Boeing Vertol & Richard D. McLain Detroit Deisel Allison

May 1974

61 AHS 30th Annual National Forum – Doc# 871- The Impact of Advanced Turboshaft Technology on T700-Powered Helicopter Systems by L.B. Veno GE

May 1974

62 AHS 30th Annual National Forum – Doc# 872- Small Turbine Advanced Gas Generators for Future Engine Requirements by Edwaed T. Johnson & Graydon A. Elloitt USAAMRDL

May 1974

63 AHS 30th Annual National Forum – Doc# 873- Balancing of High Speed Interconnect Shafting for operation Above Multiple Bending Critical Speeds by Robert H. Badgley &

May 1974

63

Jeurgen M. Tessarzik Mechanical Technology Inc. 64 AHS 30th Annual National Forum – Doc# 874- Digital

Computer Techniques for Engine/Airframe Simulation by David V. Lewis Boeing Vertol

May 1974

65 AHS 30th Annual National Forum – Doc# 883- Design, Testing and Performance of Elastometric Bearings by Warren E. Schmidt Lord Kinematics

May 1974

66 AHS 30th Annual National Forum – Doc# 884- Composite Material Geodesic Structures – A Structural-Concept for Increased Helicopter Rotor Blade Survivability by S. Pociluyko & I.E. Figge USAAMRDL and C.F. Griffin & L. Blad Lockheed-California

May 1974

67 Verti-Flite Volume 10, No. 8 August 1964 68 Aerodynamic Considerations of Rotors in Hovering and

Vertical Climb Conditions by Charles H. Kaman United Aircraft from Journal of the Aeronautical Sciences Vol 10 No 7

Jul 1943

69 AHS Meeting – A Note on the Short-Haul Commercial Transport Helicopter by Edward F. Katzenberger

Dec 21 1953

70 State of the Art Advancement in Helicopter Design Lockheed Aerogyro

Oct 1963

71 Aeroproducts Division, GM, Dayton ERs 162, 312, 315, 322, 323, 324, 327, 338, 356, 362, 370

1943

72 SBD Report No. TR 59-41 Aerial Utility Vehicle, Monthly Progress Report for May 1959 Contract# DA-44-177-TC­397

Jun 5 1959

73 AHS 28th Annual Meeting Subcommittee Chairman’s Report to Membership on Aerodynamic Sources of Rotor Noise by C.R. Cox Bell

May 1972

74 AIAA Paper No. 71-580 Hingeless Rotor characteristic at High Advance Ratios by W.A. Kuczynski Lockheed-California & D.L. Sharpe US Army Aero Research Lab (Moffitt Field)

Jun 21-23 1971

75 Lockheed 1026 Turbo-Compound Interurban Transport Undated 76 TRECOM TR 63-42 Summary Report High-Performance-

Helicopter Program Contract# DA44-177-TC-711 Sep 1963

77 TRECOM TR 64-61 High-Performance-Helicopter Program Summary Report, Phase II Contract# DA44-177­TC-711

Oct 1964

78 USAAVLABS TR 66-17 High-Performance UH-1 Compound Helicopter Maneuver Flight Test Program

Feb 1966

79 Items of Interest and Suggestions for Research by Robert R. Lynn Bell Helicopter

May 15 1968

80 AHS 30th Annual National Forum – Doc# 830- Helicopter Vibration Reduction with Pendulum Absorbers by Robert B. Taylor & Paul A. Teare Boeing Vertol

May 1974

64

81 Honeywell Document 8D-F-6 R&D Program for Fluidic Control of the Variable Deflection Thruster for Helicopter Applications

May 24 1967

82 AHS Advanced Paper Second Annual Technical Symposium – Tactical Uses of Vertical Lift Aircraft

Nov 14-16 1967

83 The Helicopter Comes of Age Boeing Helicopters Apr 3 1967 84 Utility Tactical Transport Aircraft System (UTTAS)

Boeing Mar 31 1972

85 Identification of Structural Parameters for Helicopter Dynamic Test Data Kaman

Feb 13-15 1974

86 Rotary Wing Design Methodology Kamam Mar 30-Apr6 1973

87 Test and Evaluation of a Quiet Helicopter Configuration HH-43B from Journal of the Acoustic Society of America Vol. 54, No. 5

Nov 1973

88 Report No. 24 Helicopter Stability Tests Model H-2A Landgraf Helicopter Co.

Jun 1948

89 TR ATI No. 20283 Evaluation and Tests of the Flettner­282 German Helicopter

Sep 1948

90 NASA TN D-633 An Analysis of the Flapwise Frequencies and Mode Shaped of Rotor B;\lades Having Two Flapping Hinges to Reduce Vibration Levels

Dec 1960

91 NACA TN 2309 Charts for Estimation of Longitudinal Stability Derivatives for a Helicopter Rotor In Forward Flight

Jan 22 1951

92 NACA TN 3156 Charts for Estimating Tail-Rotor Contribution to Helicopter Directional Stability and Control in Low-Speed Flight

May 1954

93 NACA TN 3236 Wind-Tunnel Studies of the Performance of Multirotor Configurations

Aug 1954

94 MIT TR 123-3 An Extended Lift Line theory for the Loads on a Rotor Blade in the Vicinity of a Vortex Contract# Now 64-0188-d

Dec 1965

95 MIT TR 133-1 An Actuator Disc theory for the Shed Wake at Low Tip Speed Ratois Contract# Now 65-139-d

Undated

96 Report No. R-585-2 The Aeroelastic Behavior of Rotary Wings in Forward Flight Contract# Now 66-0629f Kaman

Jul 1968

97 MIT TR 123-2 Approximate Solutions for Computing Helicopter Harmonic Airloads Contract# Now 64-0188-d

Dec 1965

98 USAAVLABS TR 68-22A In Flight Measurement and Correlation with Theory of Blade Airloads and Responses on the XH-51A Compound Helicopter Rotor Volume I – Measurement and Data reduction of Airloads and Structural Loads Contract# DA 44-177-AMC-357(T)

May 1968

99 USAAVLABS TR 68-22C In Flight Measurement and Correlation with Theory of Blade Airloads and Responses

May 1968

65

on the XH-51A Compound Helicopter Rotor Volume III Theoretical Prediction of Airloads and Structural Loads and Correlation with Flight test Measurements Contract# DA 44-177-AMC-357(T)

100 The TRW Approach to Complete Assessment of the Cheyenne by John F. Mosher TRW

C.A. 1967

101 Operating Problems and Experience with the Sikorsky Skycrane by Miller A. Wachs Sikorsky

1967

102 Operational Problems and Experience with Vertical-Lift Aircraft Light and Utility Helicopters by John W. Oswalt Bell

Nov 15 1967

103 Operational History and Experience with Boeing Helicopters by Howard N. Stuverude Boeing-Vertol

Nov 14-16 1967

104 AHS 27th Annual National V/STOL Forum Number 573 Army/Navy Operational Evaluation of Offshore Discharge of Containerships by LTC L. J. McConnell USArmy

May 1971

105 Technical Data Digest – Helicopter Development 1473­1943 by Thomas M. Wood

C.A. 1943

106 Institute of Aeronautical Sciences Number 109 Chordwise and Beamwise Bending Frequencies of Rotor Blades by Gabriel Horvay

Undated

107 New Markets for the S-64 Skycrane Helicopter by E.E. Gustafsson

Jan 24 1968

108 AD 627-898 An Empirical Method for Calculating the Power Required Due to Compressibility on a Single Rotor Helicopter

July 1965

HELICOPTER AIRFOILS (ROTOR BLADES) 26 1 Report R-107-4 Part II Stress Analysis of Rotor Blades by

a Tabular-Dynamic Method Goodyear Aircraft Corp. Feb 28 1946

2 Report R-107-4 Part IV Helicopter Airload Calculations Goodyear Aircraft Corp.

Mar 5 1946

3 Report R-107-4 Part II-A Stress Analysis of Rotor Blades by a Tabular-Dynamic Method (Expansion of Part II) Contract# W33-038 ac-11439 Goodyear.

Apr 24 1946

4 Report R-107-4 Part III Effects of Second-Harmonic Flapping on the Stresses of a Hinged Rotor Blade Contract# W33-038 ac-11439 Goodyear

May 2 1946

5 Report R-107-4 Part V Stress-Model Method of Determining Bending Moments in R-6 Helicopter Blades Contract# W33-038 ac-11439 Goodyear

Jun 22 1946

6 Report 230.49 Analysis of Low Frequency Rotor Blade Flutter Coupled with Vertical Pylon Motion, for a Rotor Blade Having Flapping and Lag Hinges Kellett

Jun 1947

7 Cornelius Helicopter Rotor Principles Apr 28 1946

66

8 NACA Report No. 293 Two Practical Methods for the Calculation of the Horizontal Tail Area Necessary for a Statistically Stable Airplane

Jan 1929

9 NACA Report No. 349 A Proof of the Theorem Regarding the Distribution of Lift Over the Span for Minimum Induced Drag

C.A. 1930

10 NACA Report No. 362 An Extended Theory of Thin Airfoils and its Application to the Biplane Problem

1930

11 NACA Report No. 383 On the Theory of Wing Sections with Particular Reference to the Lift Distribution

1931

12 NACA Report No. 497 Computation of the Two-Dimensional Flow in a Laminar Boundary Layer

1934

13 NACA Report No. 527 Air Flow in a Separating Laminar Boundary Layer

1935

14 NACA Report No. 546 The Effect of Turbulence on the Drag of Flat Plates

1935

15 NACA Report No. 567 Propulsion of a Flapping and Oscillating Airfoil

1936

16 NACA Report No. 613 The Variation with Reynolds Number of Pressure Distribution Over an Airfoil Section

1938

17 NACA Report No. 684 Static Thrust and Power Characteristics of Six Full-Scale Propellers

1940

18 NACA Report No. 840 Stalling of Helicopter Blades 1946 19 NACA TM No. 921 Contribution to the Aerodynamics of

Rotating-Wing Aircraft Dec 1939

20 NACA TM 907 Dynamic Stability of a Helicopter with Hinged Rotor Blades

Sep 1939

21 NACA TM 929 Aerodynamics of Rotating-Wing Aircraft with Blade-Pitch Control

Feb 1940

22 NACA TM 990 Contribution to the Aerodynamics of Rotating-Wing Aircraft Part II

Oct 1941

23 NACA TM 1312 Calculation of the Bending Stresses in Helicopter Rotor Blades

Mar 1951

24 NACA Wartime Report ARR 3G29 Theory of Self-Exciting Mechanical Oscillations of Hinged Rotor Blades

Jul 1943

25 NACA Wartime Report ARR 3I13 Theory of Mechanical Oscillations of Rotors with Two Hinged Blades

Sep 1943

26 NACA Wartime Report L4H05 Effect on Helicopter Performance of Modifications in Profile-Drag Characteristics of Rotor-Blade Airfoil Sections

Aug 1944

27 NACA Wartime Report L5C12c High-Speed Photographs of a YR-4B Production Rotor Blade for Simulated Flight Conditions in the Langley Full-Scale Tunnel

Mar 1945

28 NACA Wartime Report 5A09 Response of Helicopter Mar 1945

67

Rotors to Periodic Forces 29 NACA Wartime Report L5E10 Evaluation of the Induced-

Velocity Field of an Idealized Helicopter Rotor Jun 1945

30 NACA Wartime Report L5E23 Comparisons of Methods of Computing Bending Moments in Helicopter Rotor Blades in the Plane of Flapping

Aug 1945

31 NACA Wartime Report L6D24 Static-Thrust Investigation of Full-Scale PV-2 Helicopter Rotors Having NACA 0012.6 and 23012.6 Airfoil Sections

May 1946

31 NACA RM L54G02 Rapid Estimation of Bending Frequencies of Rotating Beams

Aug 18 1954

32 NACA TN 835 Analysis of Ground Effect on the Lifting Airscrew

Dec 1941

33 NACA TN 1083 Stalling of helicopter Blades Jun 1946 34 NACA TN 1184 Theory of Ground Vibrations of a Two-

Blade Rotor on Anisotropic Flexible Supports Jan 1947

35 NACA TN 1192 Charts Showing Relations Among Primary Aerodynamic Variables for Helicopter-Performance Estimation

Feb 1947

36 NACA TN 1812 The Application of Airfoil Studies to Helicopter Rotor Design

Feb 1949

37 NACA TN 1996 On Internal Damping of Rotating Blades Dec 1949 38 NACA TN 2226 Theoretical Analysis of Oscillations in

Hovering of Helicopter Blades with Inclined and Offset Flapping and Lagging Hinge Axes

Dec 1950

39 NACA TN 2648 Experimental Investigation of Transition of a Model Helicopter Rotor from Hovering to Vertical Autorotation

Mar 1952

40 NACA TN 2714 Normal Accelerations and Operating Conditions Encountered by a Helicopter in Air-Mail Operations

Jun 1952

41 NACA TN 2870 Power-Off Flare-Up Tests of a Model Helicopter Rotor in Vertical Autorotation

Jan 1953

42 NACA TN 2912 The Normal Component of the Induced velocity in the Vicinity of a Lifting Rotor and Some Examples of its Application

Mar 1953

43 NACA TN 3182 Manual of the ICAO Standard Atmosphere

May 1954

44 NACA TN 3376 The Effects of Control Stiffness and Forward Speed on the Flutter of a 1/10-scale Dynamic Model of a Two-Blade Jet-Driven Helicopter Rotor

Apr 1955

45 NACA TN 3844 Theory of Self-Excited Mechanical Oscillations of Helicopter Rotors with Hinged Blades

Feb 1957

46 NACA TN 3849 Analytical Determination of the Natural Coupled Frequencies and Mode Shapes and the Response

Dec 1956

68

to Oscillating Forces Functions of Tandem Helicopters 47 NACA TN 3850 Experimental Investigation of the

Langley Helicopter Test Tower of Compressibility Effects on a Rotor Having NACA 632-015 Airfoil Sections

Aug 1956

48 NACA TN 3852 Flight Measurements of the Vibrations Encountered by a Tandem Helicopter and a Method for Measuring the Coupled Response in Flight

Dec 1956

49 NACA TN 3228 Aerodynamic Investigation of a Four-Blade Propeller Operating Through an Angle of Attack Range from 0o to 180o

Jun 1954

50 NACA TN 3982 Exploratory Study of Ground Proximity Effects on Thrust of Annular and Circular Nozzles

Apr 1957

51 NACA TN 4356 Effects of Compressibility on Rotor Hovering Performance and Synthesized Blade-Section Characteristics Derived from Measured Rotor Performance of Blades Having NACA 0015 Aiorfoil Tip Sections

Sep 1958

52 NASA TN D-43 An Evaluation of Linearized Vortex Theory as Applied to Single and Multiple Rotors Hovering In and Out of Ground Effect

Sep 1959

53 NASA TN D-73 Comparison of Calculated and Measured Stall Boundaries of a Helicopter Rotor at Advance Ratios from 0.3 to 0.4

Sep 1959

54 NASA TN D-88 Wind-Tunnel Tests of a Semispan Wing with a Fan Rotating in the Plane of the Wing

Oct 1959

55 NASA TN D-89 Wind-Tunnel and Piloted Flight Simulator Investigation of a Deflected-Slipstream VTOL Airplane, the Ryan VZ-3RY

Nov 1959

56 NASA TN D-97 A Note on the Calculation of Helicopter Performance at High Tip-Speed Ratios

Sep 1959

57 NASA TN D-112 Experimental Investigation of the Pressure Fluctuations on a Flat Plate and a Cylinder in the Slipstream of a Hovering Rotor

Aug 1959

58 NASA TN D-123 Investigation of the Effects of a Guide­Vane-Rotor Combination on Inlet Total-Pressure Distortions in a Compressible Fluid

Dec 1959

59 NASA TN D-124 Static tests of an External-Flow Jet-Augmented Flap Test Bed with a Turbojet Engine

Dec 1959

60 NASA TN D-153 A Flight Study of the Conversion Maneuver of a Tilt-Wing VTOL Aircraft

Dec 1959

61 NASA TN D-175 Dynamic-Model Investigation of the Damping of Flapwise Bending Modes of Two-Blade Rotors in Hovering and a Comparison with Quasi-Static and Unsteady Aerodynamic Theories

Dec 1959

61 NASA TN D-234 Ground Effect for Lifting Rotors in Forward Flight

May 1960

69

62 NASA TN D-240 A Note on the Mean Value of Induced Velocity for a Helicopter Rotor

May 1960

63 NASA TN D-371 Natural Frequencies in bending of Twisted Rotating and Nonrotating Blades

Mar 1960

64 NASA TN D-382 Effect of Blade Cutout on Power Required by Helicopters Operating at High Tip-Speed ratios

Sep 1960

65 NASA TN D-394 Equations for the Induced Velocities Near a Lifting Rotor with Nonuniform Azimuthwise Vorticity Distribution

Aug 1960

66 NASA TN D-624 A Preliminary Study of V/STOL Transport Aircraft and Bibliography of NASA Research in the VTOL-STOL Field

Jan 1961

67 NASA TN D-789 Aerodynamics of a Fan-In-Fuselage Model

May 1961

68 NASA TN D-1548 Wind-Tunnel Tests of two Full-Scale Helicopter Fuselages

Oct 1962

69 NASA TN D-4364 Flight Investigation to determine the Effect of Longitudinal Characteristics on Low-Speed Instrument Operations

Mar 1968

70 NASA MEMO 1-31-59L Parasite Drag Measurements of Five Helicopter Rotor Hubs

Feb 1959

71 NASA MEMO 2-28-59L Comparison of Measured Flapwise Structural Bending Moments in a Teetering Rotor Blade with Results Calculated from the Measured Pressure Distribution

Mar 1959

72 NASA TT F-519 Helicopters – Calculation and Design Volume II. Vibrations and Dynamic Stability (Russian)

May 1968

73 AF TR No. 6352 Longitudinal Stability Characteristics of a Gyroscopically Stabilized Helicopter in Forward Flight

Mar 1951

74 Report CGD 443 Air and Mass Forces in the Case of Helicopter Rotors with Oblique Hinge (Supplemental Report) United Aircraft Corp.

Jul 10 1946

75 Report CGD 444 A Method for the Direct Determination of Flapping in Flight Condition with High Blade Loading

Jul 11 1946

76 Young Two-Bladed Rotor C.A. 1945 77 Basic Helicopter Design Principles Part One: Drive

Mechanisms Dec 1945

78 Analytical Comparison of Helicopter and Airplane in Level Flight by Montgomery Knight Georgia School of Technology

Jan 25 1938

79 AAF Translation No. 510 Air and Mass Forces on Helicopter Propellers with Inclined Hinge by Gerhard Sissingh (German)

Mar 30 1946

80 Report F-TS-643-RE FA-223 Helicopter Interview with Prof. Focke and Inspection of Machine (German)

Jul 3 1946

70

81 Report F-TS-687-RE Stability in Hovering of the Helicopter with Central Rotor Location by K. Hohenemer (German)

Aug 1946

82 Report F-TS-689-RE Investigation of the Influence of Rotor-Diameter, Blade Solidity, and Blade setting on the Thrust of a Rotor with Jet Propulsion by Sissingh (German)

Aug 1946

83 Report F-TS-690-RE Contributions to the Dynamic Stability of Rotary-Wing Aircraft with Articulated Blades by Sissingh (German)

Aug 1946

84 Report F-TS-1001-RE The Performance Characteristics of the Helicopter by K. Hohenemer (German)

Sep 1946

85 Report F-TS-1003-RE Static Thrust Tests of the Model Helicopter Rotor and Preliminary Research of the Model Helicopter Rotor by G. Schoppe (German)

Sep 1946

86 Report F-TS-1007-RE Investigation of the Influence of High Subsonic Velocities on the L/D of Rotary Wing Aircraft by G. Sissingh (German)

Sep 1946

87 Report F-TS-1045-RE The Power Required of the Ideal Helicopter by K. Hohenemer (German)

Jan 1947

88 Report ATI No. 19597 Stress Analysis of a Helicopter Rotor by G. von Sissingh (German)

Jun 1948

89 The Induced Drag of Any Biplane by L.V. Kerber Nov 1 1927 90 MIT – 3 Papers on Helicopter Stability and Notes May 5 1952 91 Cornell University – 2 Articles by Harold Hirsch C.A. 1949 92 Miscellaneous Articles(11) 1943-1956

HELICOPTER AERODYNAMICS/STABILITY 27 1 Report 187 Wind Tunnel Test – Model 37 Beech Aircraft Jun 24 1947

2 Some Opportunities for Progress in Aircraft Performance by George S. Schairer Boeing

Jan 20 1964

3 Advanced Transport Technology Economic Report Task IV – Summary Report Contract# NAS1-10705 and 11238 McDonnell Douglas

Undated

4 A Theory of Identification of the Parameters in the Equations of Motion of a Structure Through Dynamic Testing by William G. Flannelly & Alex Berman Kaman and Joseph H. McGarvey USAAMRDL

Mar 23-25 1970

5 Report E.S.29813 Comparison of Experimental Pressure Distributions with Those Calculated by the Neumann Program Douglas

May 16 1960

6 AF TR No. 6590 Landing Gear Vibration Oct 1951 7 Report 43209A Heavy Logistics Support Aircraft System

Optimization Study Douglas Mar 4 1963

8 Report RAC 1236 The Case for Variable Geometry by A. Wadkovsky Republic

Apr 16 1963

71

9 RASA Report 71-01 An Experimental Study of Tip Vortex Modification by Mass Flow Injection Contract# N00014­69-C-0169

C.A. Feb 1971

10 Report ASRL TR 133-2 A Routine Method for the Calculation of Aerodynamic Loads on a Wing in the Vicinity of Infinite Vortices Contract# Now 65-0139-d MIT

May 1966

11 USAAVLABS TR 65-52 A Main Power System for Shaft-Driven Heavy Lift Helicopters Contract# DA 44-177­AMC-212(T)

Oct 1965

12 Report FT-125R-69 Limited Flying Qualities and Performance of the PS-1 Seaplane

Nov 20 1969

13 Report FTD-HT-23-710-68 Short Takeoffs for Jet Aircraft by N.K. Liseytsev (USSR)

Jan 31` 1969

14 NACA RM L57E24a Some Factors Affecting the Static Longitudinal and Directional Stability Characteristics of Supersonic Aircraft Configurations

Jul 12 1957

15 NACA RM L58B06 Preliminary Study of Airplane Configurations Having Tail Surfaces Outboard of the Wing Tips

Mar 24 1958

16 NASA Memo 6-11-59L Low-Speed Investigation of the Effects of Horizontal-Tail Area and Wing Sweep on the Static Longitudinal Stability and Control Characteristics of an Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips

Jun 1959

17 Report No. D3-71019 A Power Spectral Gust Response Study of Low Level Attack Airplanes

Jan 28 1963

18 Report No. TB-969-F-1 WADC TR 56-223 Flight Evaluation of the Effect of Variable Phugoid Damping in a JTB-26B Airplane Contract# AF 33(616)-2736

Oct 1956

19 Report No. TB-757-F-9 WADC TR 54-441 Artificial Stability Installations in B-26 and F-94 Aircraft

Sep 1954

20 Report No. TB-757-F-10 WADC TR 54-442 Evaluations of Elevator Force Gradients and Types of Force Feel in a B-26

Nov 1954

21 Report No. TB-757-F-12 WADC TR 55-299 Flight Evaluations of Various Longitudinal Handling Qualities in a Variable-Stability Jet Fighter Contract# AF 33(038)­20659

Jul 1955

22 Non-Dimensional Power Curves for Aircraft in Level Flight by K. Korsak Piasecki

Undated

23 NASA TN D-217 Low-Speed Investigation of Static Longitudinal and Lateral Stability Characteristics of an

Jan 1960

72

Airplane Configuration with a Highly Tapered Wing and with Several Body and Tail Arrangements

24 NASA TN D-760 Skid Landings of Airplanes on Rocker-Type Fuselages

May 1961

25 Analysis of Thrust Due to the COANDA Phenomenon Contract# AF 61(052)-382

Oct 29 1960

26 Vertical-Gust-Alleviation System for a High-Speed Fighter Aircraft at Low Altitudes

Mar 1961

27 Report No. 133 Theoretical Aerodynamics of Flexible Wings at Low Speeds II-Two-Lobed Parawings Contract# Nonr-3728(00)

May 1 1964

28 Report No. 172 Theoretical Aerodynamics of Flexible Wings at Low Speeds IV-Experimental Program and Comparison with Theory Contract# Nonr-3728(00)

Feb 15 1965

29 Aircraft Preliminary Design Considerations of Range-Payload by Ken Coward General Dynamics/Convair

Undated

30 Pilatus Turbo Porter Model PC-6/A Aircraft Parts Catalog Undated 31 Analytical Study of a Sailwing STOL Lift System for

Limited War Aircraft VRC Sep 10 1965

32 Beechcraft MS 760 Brochure Undated 33 Pilatus Turbo Porter Model PC-6/A Specification Feb 1960 34 Pilatus Turbo Porter Model PC-6/A Aircraft Parts Catalog

(Temporary Edition) C.A. 1960

35 Pilatus Turbo Porter Model PC-6/A Aircraft Service Manual

Dec 1960 Rev Jul 1962

36 Pilatus Turbo Porter Model PC-6/A Airplane Flight Manual

Nov 26 1962

37 ASE 680646 Design and Tests of Inverting Flaps and Wing Span Flaps by Alberto Alvarez-Calderon

Oct 7-11 1968

38 ASE 730898 Propulsion Technology Advances Neede for a Quiet Supersonic transport by Richard L. Foss & Ellwood L. Bragdon Lockheed-California

Oct 16-18 1973

39 AFFTC-TR-59-38 ARDC L-28A Air Force Flight Evaluation

Jan 1960

40 Schulflugzeug Fantrainer AWI 2 VFW-Fokker (in German)

Aug 1972

41 Report LR 25180 Boxplane Configuration – Conceptual Analysis and Initial Experimental Verification Lockheed-California

Mar 30 1972

42 Report 93 Model 26 Aerodynamic Flight Test of AT-10 with 40o V Tail Beech

Aug 20 1944

43 Report 109 Model 33 Aerodynamic Wind Tunnel Test of Model 33 Beech

Aug 8 1947

44 Report 210 Model 35C Aerodynamic Rolling Jan 31 1947

73

Characteristics of Beech Model 35C with Conventional and Differential Ailerons Beech

45 Report No. T-463 UH-2 Stall Warning Flight Test Evaluation Contract# Now 65-0241-f Kaman

Apr 21 1966

46 APGS-TR-64-93 Simulated V/STOL Aircraft Operation Utilizing F-100D Aircraft

Dec 1964

47 Report ER 4223 New Transport Aircraft Lockheed Feb 1 1960 48 Report SM 10233 Study of a High-Altitude; Long

Endurance RPV Wing Structure Concept Goodyear Oct 30 1973

49 Report D180-17477-1 Liquid-Hydrogen-Fueled Aircraft May 15-16 1973 50 Report R-581/4 Airframe Structural Materials for Drone

Applications Rand Jul 1971

51 Overview of RPV Activities of the Boeing Company Apr 19 1973 52 Report SM-14025 Dimensionless Parameters for Airplane

Model Testing Douglas Mar 27 1951

53 Report 808-72-96 A Simplified Example Relating Air Transport Requirements to Aircraft Evaluation Douglas

Jan 1972

54 TAPV 60035E Fiat G95/2 Oct 1 1960 55 Report No. 209 Theoretical Aerodynamics of Flexible

Wings at Low Speeds V-Engineering Method for Estimating Parawing Performance Contract# Nonr­3728(00)

Dec 1 1965

56 SK-3287-0 Helio model U-10E Brochure Nov 1 1966

HELO AERODYNAMICS AND KAMAN K-190 28 1 Report No. 3.3 Stress Analysis of Flap Bracket and Hinge

Contract# NOa(s) 9124 Section C Item 1(a) Part 2 Kaman Oct 6 1947

2 Report No. 1.0 Structural Loads Criteria Report Contract# NOa(s) 9124 Item 1(a) Kaman

Oct 24 1947

3 Report No. 2.2 General Performance of the Model K-190­A Helicopter by the Kaman Representative Method Contract# NOa(s) 9124 Section C Item 1(a) Part 1(d) Kaman

Nov 5 1947

4 Report No. 2.3 Kaman Method of Detail Aerodynamic Rotor Performance Calculation Contract NOa(s) 9124 Item 1(a) Section C Part 1(d) Kaman

Nov 14 1947

5 Stress Analysis of Hub Assembly, Blade End Assembly and Dampers Contract# NOa(s) 9124 Item 1(a) Section C Part 2 Kaman

Nov 15 1947

6 Report No. 2.4 Kaman Representative Station Method of Helicopter Performance Calculation Contract# NOa(s) 9124 Item 1(a) Section C Part 1(d) Kaman

Nov 18 1947

7 Report No. 3.2 Load Determination and Stress Analysis of Flap Contract# NOa(s) 9124 Item 1(a) Section C Part 2

Nov 22 1947

74

Kaman 8 Report No. 2.1 Hovering Detail Analysis Contract# NOa(s)

9124 Section C Item 1(a) Part 1(d) Kaman Nov 26 1947

9 Report No. 3.1 Blade Stress at Hovering with 135 Percent Maximum Rotative Speed Contract# NOa(s) 9124 Section C Item 1(a) Part 2 Kaman

Nov 29 1947

10 Report No. 6.0 Structural Description of the Kaman Rotor Contract# NOa(s) 9124 Section C Item 1(a) Part 1(b) Kaman

Dec 1 1947

11 Report No. 3.4 Load and Stress Analysis of Rotor Controls Contract# NOa(s) 9124 Section C Item 1(a) Part 2 Kaman

Dec 8 1947

12 Report No. 7.0 Strength Summary and Operating Restrictions Contract# NOa(s) 9124 Section C Item 1(a) Part 1(f) Kaman

Dec 11 1947

13 Report No. 8.0 Loads report Contract# NOa(s) 9124 Section C Item 1(a) Part 1(c) Kaman

Dec 11 1947

14 Development of the Kinematic Focal Isolation System for Helicopter Rotors by Rodney W. Blake Bell

May 1968

15 USAAVLABS TR 68-57 Installation of a High-Reduction-Ratio Transmission in the UH-1 Helicopter Contract# DA 44-177-AMC-411(T)

May 1969

16 Bell Helicopter Military Products Reference Data May 1 1967 17 NASA TM X-3185 Wind-Tunnel Investigation of

Helicopter-Rotor Wake Effects on Three Helicopter Fuselage Models

Mar 1975

18 USAAVLABS TR 67-23 Cost Effectiveness Study of Heavy Lift Aerial Vehicles Contract# DA 44-177-AMC­205(T)

Oct 1967

19 Report No. 190V-902 Analysis of Blade C.G. and/or A.C. Offset Stabilizing System (with Viscous and Elastic Restraint) Applied to the XH-26, Pulse-Jet Helicopter Contract# AF 33(600) 15220

Feb 18 1955

20 Report No. 190V-901 Analysis of Displacement Bar Stabilizing System Applied to the XH-26 Pulse-Jet Helicopter Contract# AF 33(600) 15220

Feb 18 1955

21 WADC TR 55-407 Investigation of helicopter Stability and Control in Hovering and Forward Flight

Dec 1956

22 Progress in Dynamic Analysis and Automatic Control of Helicopters by R.P. Walton & L.G. Campbell, Jr. J.B. Rea Company Contract# AF 33(616)-108

Undated

23 Report No. 190-H-1 Investigation of Stability and Control of Small Helicopters with and Without Various Stabilizing Systems Contract# AF 33(600)-15220

Dec 31 1952

24 Unsteady Aerodynamic and Stall Effects on Helicopter Rotor Blade Airfoil Sections by Jaan Liiva Boeing Vertol

Jan 1968

75

25 Blade Tip Aerodynamics – Profile and Planform Effects by Richard F. Spivey Bell

May 1968

26 Dynamic Stall of Airfoil Sections for High-Speed Rotors by Jaan Liiva & Franklyn J. Davenport Boeing-Vertol

May 1968

27 The Effect of Advanced Propulsion on Future Rotary-Wing-type Aircraft by L.M. Graham, A.W. Schulz & H.C. Smith Bell

Jun 10-14 1968

28 Helicopter Instrument Operations in Terminal Areas by Alder P. Betti Flight Standards Service

May 14 1965

29 Present and Future Roles of the Helicopter by L.L. Douglas & J.J. Schneider Boeing-Vertol

Oct 1965

30 Control and Maneuver Requirements for Armed Helicopters by H.K. Edenborough & K.G. Wernicke Bell Helicopter (with attached sketches and photos)

May 13-15 1964

31 AHS 24th Annual National Forum – Articles # 200, 205, 207, 208, 214, 215, 217, 221, 223, 224, 225, 226, 227, 228, 229, 230, 231, 232

May 8-10 1968

32 Helicopter Propulsion Trends by C.W. Ellis, J. Acurio & J.J. Schneider Boeing-Vertol

Undated

33 Experimental Boundary Layer Study on Hovering Helicopters by W.H. Tanner Bell Helicopter & P.F. Yaggy Ames Research Center

May 11-13 1966

34 Operating History and Experience with Boeing Helicopters by Howard N. Stuverude Boeing-Vertol

Nov 14-16 1967

35 The Boundary Layer of the Hovering Helicopter by W.H. Tanner Bell Helicopter & P. Buettiker Arlington State College

C.A. 1967

36 SAE 680672 Structural Fatigue Considerations in the Design of Rotary-Wing Vehicles by H.G. Smith Hughes Tool

Oct 7-11 1968

37 SAE 680673 Vulnerability and Crashworthiness in the Design of Rotary Wing Vehicle Structures by Melvin J. Rich Sikorsky

Oct 7-11 1968

38 Stowed Rotor Assault Transport Parametric Study Boeing-Vertol

Undated

39 Field Repairable-Expendable Main Rotor Blade by A.S. Falcone & J.E. Miller Kaman

1977

40 Report No. R-442 10-Ton Intra-Theater Transport Kaman Oct 24 1962 41 The Pressure-Jet Helicopter Propulsion System by J.B.

Nichols The Aerospace Corp. Sep 1972

42 An Evaluation of Some Important Stability Parameters that Influence Helicopter Flying Qualities by Alfred Gessow & Kenneth B. Amer Langley

Undated

43 WADC TR 58-54 Part I A Study of the Frasibility of Using a Semi-Rigid or Articulated Rotor System on a Tilt-Wing VTOL Aitcraft

Oct 1957

76

44 AGARD-CP-121 Advanced Rotorcraft Volume I Sep 20-23 1971 45 AGARD CP No. 31 Helicopter Propulsion Systems Jun 1968

ROTORS 29 1 Report No. 204-099-702 Aerodynamic Data for Use in the

Selection of Design Parameters for Semi-Rigid Multi-Blade Rotors Contract# AF33(600)-30299 Bell

Mar 8 1957

2 Report no. 47-980-113 Initial Flight test evaluation of X47-120-400 Three-Bladed Rotor Contract# AF33(600)­30299 Bell

Apr 1 1957

3 Report No. 299-099-072 Proposal for the Construction and Test of an Experimental Rotor Blade Suitable for Operation at High Tip Mach Number Bell

Nov 6 1957

4 Report No. 299-099-086 A Proposal for an Applied Research Program in the Field of Helicopter Aerodynamics Bell

Apr 7 1958

5 Report No. 8011-099-002 The Weights of Very Large Rotors for Nuclear Powered Helicopters Bell

Apr 23 1959

6 Report No. 299-010-051 Proposal for Extended Studies of the Three-Bladed Semi-Rigid Rotor System on the HU-1 Helicopter Bell

Jun 15 1959

7 Report No. 299-010-050 Proposal for Developing a Means of Measuring Rotor Loads Bell

Feb 14 1958

8 Report No. 6751 Proposal for Forward Flight-Tests of High Speed Rotor Blades McDonnell

Apr 15 1959

9 Report No. 1078 Charts for Estimating Blade Stall for Jet Rotors Contract# AF33(038)-937 McDonnell

Mar 18 1948

10 Report No. SM-18310 Preliminary Report on Some Aerodynamic Problems of Vertical Capability Transport Douglas

Apr 4 1954

11 Report No. SM-18294 Vertical Capability Transport – Model 1845 Douglas

Mar 24 1954 Rev. Apr 9 1954

12 WADC Report 52-256 Low-Range Air-Speed Indicator for Helicopters Contract# AF33(038)-22265

Oct 1952

13 NACA TN 2062 Dynamic Similitude Between a Model and a Full-Scale Body for Investigation at Full-Scale Mach Number

Mar 1950

14 Report No. C-266 Wind-Tunnel Tests of a 0.10-Scale Model of the HRP-2 Helicopter Without Rotors Part II – Longitudinal and Lateral Characteristics with Revised Afterbody

Oct 1949

15 Research Report #23 An Application of Boundary Layer Control to Rotating Blades Mississippi State Univ.

May 30 1959

16 Report No. 240 On the Design of Models for Helicopter Research and Development Princeton Univ.

Oct 1953

77

17 Report No. 338 Instrumentation of a Tandem Helicopter for Static and Dynamic Stability and Control Flight Tests Princeton Univ.

Mar 1956

18 Report No. SER-2187 Analytical Solution of Static Longitudinal Trim in Hovering and Forward Flight Contract# AF33(038)-14807 Sikorsky

Apr 8 1953

19 Proposal for Developing Optimum Rotor Blades Prewitt Apr 27 1959 20 Report No. 16-X-2 PiAC-16 Helicopter with Shrouded

Propeller for Torque Correction Mar 25 1957 rev. Apr 11 1957

21 Report No. PR-198 Proposal for a Flight Test Program to Determine the Effect of Pulsating Aerodynamic Pressures on Tandem Rotor Helicopter Vibrations Vertol

Dec 6 1957

22 Report No. 121X90-5 Proposal to Determine a Method for Specifying Design Loads Associated with Flight Maneuver and Skid Landing Maneuver Criteria Kellett

Jan 1959

23 Report No. F-TS-1003-RE Static Thrust Tests of the Model Helicopter Rotor and Preliminary Research of the Model Helicopter Rotor by G. Schoppe (from German)

Sep 1946

24 An Investigation of the Experimental Aerodynamic Loading on a Model Helicopter Rotor Blade Contract# NAw-5983 MIT

Feb 1951

25 Report No. 510 Air and Mass Forces on Helicopter Propellers with Inclined Hinge by Gerhard Sissingh (from German)

Mar 30 1946

26 Report No. F-TS-689-RE Investigation of the Influence of Rotor-Diameter, Blade Solidity, and Blade Setting on the Thrust of a Rotor with Jet Propulsion by Sissingh (From German)

Aug 1946

27 WADC TR 58-124 A Design Investigation of a Propeller Air Flow Measurement System

Apr 1958

28 Report No. 30—929-111 Model Tests on Underslung Rotor Bell

Nov 8 1944

29 Application of Boundary Layer Control to Rotor Blades Progress Reports for Sep 1953, Nov 1953, Mar 1954

Oct 17 1953

30 Business Proposal for a One Man Ultra-Light Helicopter United Technical Industries

Apr 1983

31 Development of Air Mobility by Helicopter Second Edition Boeing-Vertol

Aug 1 1968

32 Helicopter Range & Speed Extension by Aerial Towing with Fixed-Wing Aircraft

May 29 1969

33 The “Heliocoupe” A New Light Helicopter Design Helicopter Research Lab. Dayton, OH

Feb 1946 Rev. Mar 4 1946

34 Report No. AN 01-230HB-2 Pilot’s Flight Operating Instructions for Army R-5A/Navy HO2S-1 Helicopters

Feb 25 1945

35 Report No. AN 01-230HB-1 Erection and Maintenance Instructions for Army R-5A/Navy HO2S-1 Helicopters

Apr 25 1945

78

36 Report No. AN 01-230HB-4 Pilot’s Parts Catalog for Army R-6A/Navy HOS-1 Helicopters

Feb 20 1945

37 Summary of Rotary Wing Projects of Aircraft Projects Section ( by Models) TSEOA-5 AMC

Jan 1945 rev. Feb 1947

38 R 420-71-LC-14b Helicopter Propulsion System Study Contract#AF33(038)-22185 Thermal Research& Engineering Corp.

Sep 1952

39 The Impact of technology on Payloads of Very Large Helicopters by Lewis G. Knapp, Wilfried Meier & David Unsworth Sikorsky

Sep 23-25 1969

40 WADC TR 57-583 Part I Helicopter Configuration and Propulsion Systems Study Part I. Statistical Weight Analysis

Nov 1957

41 Cost Effectiveness Comparison of Heavy Lift Helicopter Systems HTC

C.A. 1970

42 The STORC Approach to the Helicopter Ferry Problem by J.B. Nichols Hiller

Undated

43 Hughes Hot Cycle Presentation Undated 44 The Hot Cycle Propulsion System Research Program by

K.B. Amer HTC Undated

45 The Hot Cycle Flying Crane Helicopter by Harvey O. Nay & Robert J. Sullivan HTC

Jan 1963

46 Jet Propelled Rotor for Helicopters Undated 47 ER No. 63-24 Tip Turbojet Powered Heavy-Lift Rotor

System Hiller Undated

48 ER No. 62-66 1962 Flying Crane Design Study Hiller Jun 1962 49 Report No. 58-142 Proposal for the Development of Large

Transport and Crane Helicopters Powered by Rotor Tip Mounted Turbojets Hiller

Nov 1958 rev.1 Jul 1959

50 The Application of Tip Turbojets to the Solution of Design and Operating Problems of Large Helicopters by John B. Nichols Hiller

May 12 1960

51 Summary Report on New family of V.T.O.L. Vehicles Mar 1963 52 Report No. 29472-7 Proposal for Development of

Aerocrane (A Lightweight, Very High Payload Flying Crane) Ryan

Jul 15 1966

53 Environmental Effects on Rotor Tipjet Propulsion by E.R. Sargent, R.M. Lockwood & M.F. Gates Hiller

Oct 1956

54 Tip Turbojet Powered Heavy Lift Aerial Vehicle Hiller & Continental

Mar 1962

55 Report No. 62-39 Tip Turbojet Powered Heavy Lift Aerial Vehicle Part I: Airframe Program Hiller

Mar 1962

56 Report No. 62-12 Proposal for Flight Demonstration of Rotor Tip Mounted Turbojets Hiller

Jan 1962

57 Report AMCA-70-001 Aerial Very Heavy Lift Concepts for the 1990 Army Volume I – Basic Report

Nov 1969

79

58 A Flying Crane Readily Convertible to a High Speed VTOL Transport – Slide Presentation

Undated

59 Paper No. 20 Research and Development on Rotors with Tip Jet Drive in Germany by Christoph Fischer Dornier

Sep 1971

60 AHS 27th Annual V/STOL Forum Paper 552 Size Effects on the Design of Large Rotor Systems by Henry G. Smith HTC

May 1971

61 AHS 27th Annual V/STOL Forum Paper 561 Turbofan Engine Considerations for Reaction Drive Rotors by R.J. Sullivan HTC

May 1971

62 Optimization of Design Data for Reaction Drive Helicopters by Werner Goller Dornier

Jan 1970

HELICOPTER/ROTOR AERODYNAMICS 30 1 Helicopter Development 1939-1950 Volume 3 (original

Manuscript) 1954

2 The Domain of the Helicopter by Raoul Hafner, F.R.Ae.S Bristol Aeroplane Co., Ltd.

Oct 1954

3 Proposal to Develop a Small VTOL Remotely Piloted Vehicle (original) probably by Lindenbaum

Undated

4 Miscellaneous Articles – Early Helicopters Various 5 Hover Tests of a Model H-Force Rotor by H.R. Velkoff

Ohio State Univ. Sep 8-11 1981

6 A Note on Rotary Wing Hovering and Takeoff Performance, Data Acquisition and Analysis by John C. Kidwell USArmy Test & Eval. Command

Undated

7 Preliminary Study of the H-Force Rotor by Henry R. Velkoff & Thomas W. Parker Ohio State Univ.

Oct 22-24 1980

8 FAA-P-8100.1 Rotorcraft Master Plan Sep 1987 9 Air-Jet Helicopter Air-Jet Development Corp. Undated 10 Piasecki – Miscellaneous Information 1956-1959 11 The Boeing Fiberglass Blade Manufacturing Story

Brochure Undated

12 Helicopter Research & Development Conference Bell May 16-17 1961 13 DH_2011 Experimental Helicopter Undated 14 Report No. 150-FT-1004P Proposal for a Variable Sweep,

Oscillating Pitch Rotor Blade Airfoil Test Program HTC Apr 1972

15 Report No. 150-A-1005P Optimum Pitch Rotor System Wind Tunnel Model Test HTC

Mar 1972

16 Report 150-A-1006P Aerodynamic Testing of Bidirectional Airfoil Sections

C.A. 1972

17 Current Status of the helicopter by Henry R. Verkoff Ohio State Univ.

Sep 21 1967

18 Selected Data from HTC-AD OPR Computer Studies Undated 19 Optimum Pitch Rotor (OPR) Presentation Handout HTC Undated

80

20 A Nonlinear Aeroelastic Loads Analysis of Rotary Wings by A.Z. Lemios Kaman

Undated

21` Calculated and Measured Thrust, Torque and Performance of a Helicopter Rotor by P.E. Hemke, Louis Levoy & Wm. E. Wayman

Undated

22 Report No. 1-001-003 Theoretical Background for the Vaughen Helicopter Rotor System

C.A. 1958

23 Report No. 2-000-001 Technical Proposal Phase I Development Program for the Vaughen Rotor System

C.A. 1958

24 Report No. 2-000-001R Revised Proposal Phase I Development Program for the Vaughen Rotor System

C.A. 1958

25 Vaughen Aircraft Corp. Correspondence Concerning Their Rotor System

1958

26 Instrument Flight Investigation in Helicopters by Owen Q. Niehaus Bell

Undated

27 The Hiller “L” Rotor Control and Stability Augmentation System

May 1963

28 Report No. R-309 Advanced Rotor Configuration Research Boeing-Vertol

Feb 15 1963

29 Report No. 659 Aerodynamic Characteristics of Helicopter Rotors Princeton Univ.

Dec 1963

30 Reports and Translations No. 1021 Survey on German Research and development of Rotary Wing Aircraft by G. Sissingh (from German)

Aug 1 1948

31 FSTC-HT-23-1472-72 Helicopter Design by V.N. Dalin (from USSR)

1971

32 F-TS-9747/V The Aerodynamic Design of Helicopters by B.N. Yur’yev Part I of II

Apr 1960

33 F-TS-9747/V The Aerodynamic Design of Helicopters by B.N. Yur’yev Part II of II

Apr 1960

34 Report No. G-71 Interim ER on Internal Combustion Engines and Hose-Cable Assemblies for a Tethered Antenna Supporting Helicopter Contract# AF 30(602)-675 Kaman

Aug 1 1954

35 USAAMRDL-TR-74-56 Analysis of Unmanned, Tethered, Rotary-Wing Platforms

Jul 1974

36 Report No. A.A.E.E./Res/264 Aeroplane and Armament Experimental Establishment The Low Speed Performance of a Helicopter UK Min. of Supply

May 15 1952

37 R & M No. 1730 The Flight of a Helicopter Nov 28 1935 38 Tech. Note AERO.2131 Helicopter Behavior in the Vortex

Ring Conditions UK Royal Aircraft Estab. Nov 1951

39 AHS SW Regional Meeting Turning a Rotor into Profit by Harry W. Mitchell Bell

Oct 22 1954

81

40 AHS 21st Annual Forum A Study of the Turbine Integrated Geared Rotor for the Heavy-Lift Helicopter by Robert B. Bossler, Jr. Kaman

May 12-14 1965

41 AHS 25th Annual Forum Paper No. 341 A Comparison of Dynamically Scaled Model Rotor Test Data with Discrete Azimuth Aeroelastic Stability theory by Charles F. Niebanck Sikorsky

May 14-16 1969

42 AHS 33rd Annual Forum Paper 77.33.12 The Army’s Improved Main Rotor Blade for the AH-1 Helicopter by Paul F. Maloney Kaman, Larry G. Dite Army Avn Syscom, & Robert D. Powell USAAMRDL

May 1977

43 AHS 34th Annual Forum Paper 78-36 Filament Wound Main Rotor Blade – The Army’s New Production Blade for the AH-1 by Mark L. White Kaman Aerospace

May 1978

44 AHS 35th Annual Forum Paper 79-38 Rotorshaft Torquemeter by Robert B. Bossler, Jr. Kaman

May 1979

45 AHS 35th Annual Forum Paper 79-40 Ground Test Vehicle Testing by H.D. Jones USAA R&D Command

May 1979

46 AHS 35th Annual Forum Paper 79-43 Certification of Composites in Civil Aircraft by R. Allen & J.R. Soderquist FAA

May 1979

47 AHS 35th Annual Forum Paper 79-49 Helicopter Component Environmental Vibration Testing by Dr. Sam T. Crews USAA R&D Command

May 1979

48 NASA TN D-2628 Wind-Tunnel Investigation of a Lifting Rotor Operating at Tip-Speed Ratios from 0.65 to 1.45

Feb 1965

49 Rigid Rotors vs. Hinged Rotors for Helicopters by Bertram Kelley

Mar 25 1963

50 AIAA Paper No. 64-784 Technology Contributions of the CH-53A Weapons System Development Program by Edward S. Carter, Jr. Sikorsky

Sep 21-23 1964

51 Lockheed Rigid Rotor Helicopter Article and 2 Blueprints 1963-1965 52 Fiat 7002 Helicopter – Letter and Notes Jan-Feb 1960 53 Helicopter Articles and Other Papers Various

HELICOPTER VIBRATION, MISC. HELICOPTERS 31 1 Alouette Helicopter Brochures (6) Various

2 Helicopter Brochures (13) Various 3 FT-58R-67 Navy Evaluation of the Fairchild-Hiller Model

FH-1100 Light Turbine-Powered Helicopter NATC Sep 22 1967

4 Advanced Commercial Helicopter Presentation Summary Boeing-Vertol

May 1967

5 AHS 23rd Annual Forum Paper No. 113 The US Army Hueycobra - Configuration and Design Considerations by Charles M. Seibel Bell

May 11-13 1967

6 AHS 23rd Annual Forum Paper No. 112 The Dollar Value May 11-13 1967

82

of Empty-Weight Control in Helicopters by Kenneth B. Amer & Robert J. Sullivan HTC

7 AHS 23rd Annual Forum Paper No. 111 Methods for Improving Flying Qualities of Compound Helicopters by W.E. Blackburn Kaman

May 11-13 1967

8 Report SER-50174 Sikorsky High Performance Helicopter Oct 1961 9 USAAMRDL TR 71-23 Advanced Anti-Torque Concepts

Study Jul 1971

10 USAAMRDL TR 71-44 Advanced Anti-Torque Concepts Study

Aug 1971

11 Report No. R-140A KAMAN Model K-600 Local Crash Rescue Helicopter for the USAF

Dec 1 1956

12 Report No. AD872906 AH-56 Cheyenne Control Augmentation System Study

Jul 1970

13 WADC TR 55-437 An Investigation of the Handling Characteristics of a Sikorsky H-19 Helicopter Equipped with Various Mechanical Stabilizers – Part I Analytical Evaluation of Stabilizers

May 1957

14 Report No. R-140C Detail Specification KAMAN Model K-600 Crash rescue Helicopter for the USAF

Sep 5 1957

15 Practical Instrument Flying in the Helicopter by Joseph A. Cannon & Owen A. Niehaus Bell helicopter

Undated

16 Report No. SER-3309 Model Specification – Model H-19B (MDAP) Helicopter 12-Place, Single-Engine Contract# AF33(600)-22310 Sikorsky

Nov 17 1953

17 AHS (23rd) National Forum The US Army Hueycobra Configuration and Design Considerations by Charles M. Seibel Bell

May 10-12 1967

18 Report No. 56-66 Proposal to the USAF – Local Crash Rescue Helicopter Hiller

Jun 1956

19 Report No. SER-2556 Summary Report – Long Range Helicopter Design Study Contract# AF33(616)-2628

May 27 1955

20 Report No. 80X-80-1 Proposal for a Study to Investigate the Possibility of Obtaining Substantial Improvement in Range and Cruise Speed Performance for Helicopters Contract# USAF PR 383905

Apr 1954

21 Report No. 1081 Calcul Des Forces Aerodynamiques Instationnaires Sur Les Pales D’un Rotor D’Helicoptere (in French)

1972

22 DOD Contract DA 44-177-TC-420 with Bell helicopter for a Preliminary Design Study for a Two-Place Helicopter

Mar 29 1957

23 AIAA Paper No. 71-994 The Heavy Lift Helicopter Program – An Advanced Technology Solution to Transportation Problems by Ben Tencer & J.P. Cosgrove Boeing

Oct 25-28 1971

83

24 Paper No. 3 The Developing Technology and Economics of Large Helicopters by John J. Schneider Boeing-Vertol

Sep 16-19 1980

25 Report No. RD46-310000-1 Final Report on Preliminary Design Study of Optimum Army Two-Place Observation Helicopter Contract# DA 44-177-TC-419

Aug 30 1957

26 Acoustic Effects of Rotor-Wake Interaction During Low-Power Descent by Bruce D. Charles

May 6-7 1975

27 The Bert Kelley Award Technical Presentations for 1968 1968 28 Report No. 190-F-1 Preliminary Design Study – Army

Two-Place Helicopter – Final Summary Report Nagler Helicopter Co.

Sep 6 1957

29 USAAVLABS TR 68-42 An Analytical and Model Test Research Study on the Kaman Dynamic Antiresonant Vibration Isolator (DAVI) Contract DA 44-177-AMC­391(T)

Nov 1968

30 USAAVLABS TR 68-60 Studies of Helicopter Rotor Noise Contract# DAAJ02-67-C-0023

Jan 1969

31 USAAVLABS TR 70-30 The Exploratory Development of the Three-Dimensional Dynamic Antiresonant Vibration Isolator for Rotary-Wing Application Contract# DAAJ02­69-C-0003

Aug 1970

32 Assorted Blueprints Various

ROTORS, AERIAL UTILITY VEHICLE 32 1 Report No. 299-099-086 A Proposal for an Applied

Research Program in the Field of Helicopter Aerodynamics Bell

Apr 7 1958

2 Report No. 299-099-110 A Proposal to Experimentally Determine High Speed Rotor Performance, Including Effects of Stall and Compressibility, and Comparisons with Theory

Apr 14 1959

3 Report No. 299-099-113 An Analytical Study of the Longitudinal Stability of Tandem Rotor Helicopters Contract# BuAer NOa(s) 58-534-c Bell

Jul 13 1959

4 Report No. 299-099-137 Final Report – Analytical and Experimental Studies of the Flying Qualities of Tandem Rotor Helicopters Contract NOa(s) 58-534-c Bell

May 25 1960

5 Report No. 204-099-928 Model XH-40 Revised Design Three Bladed Rotor Ground and Flight Tests Contract# AF 33(600)30299 Bell.

Apr 16 1959

6 Report No. 204-099-929 Investigation of Rotor Behavior Following Throttle Chop – YH-40 Helicopter Bell

Jul 10 1959

7 Report No. PR-191 A Study of Boundary Layer Control to Reduce Helicopter Download Vertol

Sep 4 1957

8 Report No. PR-225 Program for the Improvement of the Static Longitudinal Stick Position vs. Forward Speed

Feb 19 1958

84

Characteristics of Tandem Rotor Helicopters Vertol 9 Report No. PR-267 Proposal for Flight Test and Evaluation

of Hydromechanical Stability Augmentation System Vertol

Sep 22 1958

10 Wind Tunnel Tests on Four Model Helicopter Rotors in Vertical Descent by Walter Castles, Jr. & Robin B. Gray Georgia Institute of Technology Contract# NAw 5527

May 1960

11 Report No. PR-106 Proposal for the Advancement of Techniques for V/STOL Lift and Propulsion Systems Vanguard Air & Marine Corp.

Aug 31 1961

12 SBD Report No. TR 59-77 Aerial Platform Monthly Progress Report for Sep 1959 Contract# DA-44-177-TC­397 Curtiss

Oct 1 1959

13 SBD Report No. TR 59-87 Aerial Platform Monthly Progress Report for Oct 1959 Contract# DA-44-177-TC­397 Curtiss

Nov 6 1959

14 Report No. SM-18311 Helicopter Vibration Model 1845 Douglas

Apr 9 1954

15 Report No. ARD-213 Static Lift Characteristics of Jet Slots – A Clarifying Study of the External Ejector –Final Report Contract# Nonr 2428(00) Hiller

Oct 15 1958

16 ER No. 59-25 21 Ton Payload Flying Crane Helicopter for Army Missions Hiller

Mar 1959

17 ADC Report No. 520-2/R34/46 Monthly Progress Report on the Aerial Utility Vehicle Apr 1 – Apr 30 Contract# DA-44-177-TC-397 Aerophysics

May 5 1958

18 ADC Report No. 520-2/R35/46 Monthly Progress Report on the Aerial Utility Vehicle May 1 – May 31 Contract# DA-44-177-TC-397 Aerophysics

Jun 5 1958

19 ADC Report No. 520-2/R36/46 Monthly Progress Report on the Aerial Utility Vehicle Jun 1 – Jun 30 Contract# DA­44-177-TC-397 Aerophysics

Jul 8 1958

20 ADC Report No. 520-2/R37/46 Monthly Progress Report on the Aerial Utility Vehicle Jul 1 – Jul 31 Contract# DA­44-177-TC-397 Aerophysics

Aug 7 1958

21 ADC Report No. 520-2/R38/46 Monthly Progress Report on the Aerial Utility Vehicle Aug 1 – Aug 31 Contract# DA-44-177-TC-397 Aerophysics

Sep 9 1959

22 ADC Report No. 520-2/R31/46 Monthly Progress Report on the Aerial Utility Vehicle Feb 1 – Feb 28 Contract# DA-44-177-TC-397 Aerophysics

Mar 5 1958

23 TREC TR 60-70 Study of the VTOL Downwash Impingement Problem Contract# DA-44-177-TC-689

Nov 1960

24 WADC Technical Note 58-98 AD-151146 Investigations Jan 1958

85

Toward the Development of an Aerodynamic Strip Analysis for Single Rotation Propellers Operating at Low Airspeeds and/or Low Advance Ratios

25 Preliminary Report – Phase II Evaluation of XV-1 Convertiplane

Jun 1956

26 Report No. 230.58 Model XR-17 A determination of the Rotor Horsepower Required for Hovering Flight Including the Effects of Varying the Pitch, Chord and Airfoil Section Along the Span Kellett

Apr 1947 Rev. Apr 30 1948

27 Report No. 124X90-3 Proposal for Low-Cost Fuselage Construction Using Reinforced Plastics Kellett

Apr 1958

28 Preliminary Presentation of Results on VTOL Operational Limitations Due to Downwash Effects Contract# Now 60­0450-f

May 1 1961

29 Report No. H-123-3 Stability of Rotor Blade Flapping Motion Contract# NOa(s)-3703 McDonnell

Jan 23 1946

30 ER 1079 Charts for Estimating the Autorotative Performance of Jet Rotors Contract# AF 33(038)-937 McDonnell

Mar 18 1949

31 ER 1100 An Autorotative Performance Study of the Model 38 Flyable Test Stand Contract# AF 33(038)-937 McDonnell

Mar 18 1949

32 Report No. SER-74 Induced Velocity in Level Flight Contract# W535 ac-29005 Sikorsky

Dec 22 1944

33 Report No. SER-1524 A Comparison Between Modified Tandem and Full Tandem Type Helicopters Sikorsky

Mar 17 1947

34 Report No. 22-A-05 Report on Methods and Computations Used in Selecting Rotor Physical Characteristics and Efficiencies for the H-21 Helicopter Contract# AF 33(038)-12881 Piasecki

Apr 1951

35 Report No. RP-42 Helicopter Stability Criteria Cessna Jan 9 1959 36 Report No. DR-306 Engineering Flight Test Evaluation of

Doman Rotor System Contract# NOas58-679-c Doman Mar 30 1959

37 Limited Flight Evaluation of the English Fairey Rotodyne by Charles C. Crawford & Maj. Walter J. Hodgson

Undated

HELICOPTER TOWING & RANGE EXTENSION 33 1 Helicopter Towing Presentation Including Slides, Notes

Photos, Vugraphs & Background Data 1998

2 Report No. M-E109 Mid Air Cargo Transfer to Rotary Wing Aircraft All American Engineering Co.

Jan 1967

3 AHS 5th Annual Western Forum A Study of the Attainable Range of Helicopters by Abraham C. Adler & Helen S. Holm Cornell

Sep 25-26 1958

4 Report No. 2-809 Analysis of Rotary Wing Gliders as a Jan 1949

86

Type Eastern Rotorcraft 5 Memorandum RM-3809-PR Parasiting Versus Aerial

Refueling for Support of Combat Aircraft Rand Corp. Mar 1964

6 UH-2C Brochure Kaman 1967 7 Report NO. SER-1906 Aerodynamic Analysis of a

Helicopter Towed as a Glider Contract# M 6549-2 Sikorsky

Jan 19 1949

8 Helicopter Range Extension by Means of Aerial Towing and Hock-On by B.T. Wolfson & B. Lindenbaum ARDC WPAFB

Undated

9 Proposed Helicopter Towing Arrangements Various 10 Report No. P-149 Stress Analysis – Helicopter-In-Flight

Pick-Up Kit Contract# AF 33(600)-18639 All American Engineering

Apr 1953

11 Report No. TR 11-100 Study of “Pick-A-Back” Operation of an H-5H Helicopter on a C-119B Airplane Part I: Theory and Design Contract# AF 33(616)-239 Thieblot Aircraft Co.

Oct 10 1957

12 Report No. TR 11-100 Study of “Pick-A-Back” Operation of an H-5H Helicopter on a C-119B Airplane Part II: Wind Tunnel Tests Contract# AF 33(616)-239 Thieblot Aircraft Co.

Oct 10 1957

13 A V/STOL Cargo/Transport Glider System by B. Lindenbaum

Mar 1972

14 A V/STOL System for Light & Medium Intratheater Transport (LIT/MIT) by B. Lindenbaum

Mar 1972

15 Vertical Take-Off and Landing “Glider” Concept Weekly Activity Report

Jul 26-30 1971

16 “Mother-Daughter” Operation of Helicopter with Airplane to Improve Rescue Capability Proposal Paperwork by B. Lindenbaum

1967-1968

17 Helicopter Towing Notes Lindenbaum/Kaman/Lockheed 1981 18 LIT (Light Intratheater Transport) Tilt Wing and “Glider” 1971 19 V/STOL Towed Glider notes from AHS Meeting Jun 13 1975 20 VTOL Glider – Miscellaneous Notes Various

21 Report No. ER 9736 “Project Dock” A Self-Contained System for Launch, Control and Recovery of Drones Lockheed-Georgia (2 copies plus notes)

Jan 1968

22 Canadair CX-84 VTOL Glider Concept Jul 20 1971 23 B36/F84E Photos & Negatives Undated 24 Miscellaneous Articles and Photos Various

HUGHES HOT CYCLE ROTOR/WING COMPOSITE AIRCRAFT

87

34 1 Report No. HTC-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 2 Performance Data HTC

May 1966

2 Report No. HTC-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 3 Propulsion System HTC

May 1966

3 Report No. HTC-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 4 Weight and Balance HTC

May 1966

4 Report No. HTC-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 6 Structures Part I HTC

May 1966

5 Report No. HTC-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 6 Structures Part II HTC

May 1966

6 Report No. HTC-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft section 11 Results of Model Testing HTC

May 1966

7 Report No. HTC-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 16 Preliminary Model Specification HTC

May 1966

8 Report No. HTC-66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 16 Parametric Studies and Alternate Configurations HTC

May 1966

9 Report No. HTC-66-10 TR Hot Cycle Rotor/Wing Composite Research Aircraft Program Summary HTC

May 1966

10 Report No. HTC 65-15 Volume III Appendices G and H Summary TR Rotor/Wing Concept Study HTC

Sep 1965

HELICOPTERS 35 1 WADC TR No. 55-437 Part II An Investigation of the

Handling Qualities of a Sikorsky H-19 Helicopter Equipped with Various Mechanical Stabilizers Contract# AF 33(616)-2780

Jan 1958

2 Report No. 102X90-4 An Investigation of the Handling Qualities of a Tandem Rotor Helicopter (H-21) Equipped with a Gyroscopic Stabilizing System Contract# NOas 56­796-c Kellett

Aug 1 1958

3 AFFTC-TN-57-13 Effect of Gross Weight and Center of gravity Location on Dynamic Stability of a Tandem Rotor Helicopter in Forward Flight

Jun 1957

4 Wing-Rotor Interaction by Robert R. Lynn Bell 1966 5 Investigation of Helicopter Stability and Control in Feb 28 1956

88

Hovering and Forward Flight Final Report Contract# AF 33(616)-108

6 Convertawings Inc. “Quadrotor” Concept Paper Jan 9 1958 7 The Influence of Blade Flapping Restraint on Dynamic

Stability of Low Disk Loading Prepeller-Rotors by Maurice I. Young & Roman T. Lytwyn Boeing-Vertol

May 10-12 1967

8 AFFTC-TN-58-1 Flight Evaluation of Directional Stability and Control of Kaman K-600 with Various Empennage Configurations and Stability Augmentation

Feb 1958

9 Report No. NRL 4621 Velocity Tests of NRL Valve Pulsejet and Whirling Loss Evaluation

Nov 4 1955

10 Report No. R-585 The Aeroelastic Behavior of Rotary Wings in Forward Flight Final Report Volume I-Analysis Contract# Now 64-0488f Kaman

Undated

11 Chinook Crane – The Boeing Model 297 Heavy Lift Helicopter Brochure

Undated

12 New Control Criteria for VTOL Aircraft by Robert R. Lynn Bell

Aug 1962

13 Fuselage Vibration Prediction Boeing 1965 14 Performance Potential of Rotor Blade Inboard

Aerodynamic Devices by Maurice I. Young & Jaan Liiva Boeing

Jun 22-24 1966

15 Report No. 395 Stability and Control of Tandem Helicopters Phase III & IV Static and Dynamic Lateral Stability and Control Contract# Nonr-27024 Princeton Univ.

Jul 1957

16 Heavy Lift Helicopter Technology Assessment 1968 Lockheed-California

1968

17 Report No. FT23-4R-64 Military Research Evaluation of the Lockheed XH-51A Rigid Rotor Helicopter Final Report

Jan 7 1964

18 The Coming Revolution in Aeronautics with VTOL/RLS Presentation Bell

May 18 1966

19 FanJet Drive Systems for Heavy Lift Helicopters HTC Undated 20 Technology Background Fanjet Drive HLH Presentation May 8 1969 21 Proposed Areas for Rotorcraft Development Aircraft

Laboratory C.A. 1956

22 Summary of Parametric Studies for Flying Crane Helicopters

Aug 1957

23 Development of the Helicopter Brochure Lockheed-California

1966

24 Extending Helicopter Speed Performance Brochure Lockheed-California

C.A. 1967

25 Paper No. 782 Heavy Lift VTOL – Effect of Weight and Size on Productivity by J.E. Fuller & M.L. Marquis Sikorsky

May 5-8 1969

89

26 Garrett RPV Presentation Undated 27 Air Force Long Range R&D Program for Rotary Wing

Aircraft Presentation Apr 1954

28 Report on Helicopter Developments in Germany by R.H. Prewitt

May 1945

29 NAVWEPS 00-80T-88 (ATC Manual 51-2) Helicopter History and Aerodynamics Manual

1961

30 DAVI (Dynamic Antiresonant Vibrator Isolator) Brochure Kaman

Undated

31 Proposal No. 35-4 Unsolicited Proposal for the development of the Helicycle Vehicle by Peter R. Payne

Apr 12 1968

32 AFFTC-TR-60-2 Appendix III YHO-2HU Air Force Flight Evaluation

May 1960

33 Summary Report on New Family of VTOL Vehicles Brochure L.C. McCarty

Mar 1963

34 PB 121097 Rotary Wing Aircraft Handbook and History Contract# W33-038 ac-21804(20695) Vol. 5 Weight and Balance

1954

35 PB 111390 Rotary Wing Aircraft Handbook and History Contract# W33-038 ac-21804(20695) Volume 6 Aerodynamics and Performance of Helicopters

1954

36 PB 111289 Rotary Wing Aircraft Handbook and History Contract# W33-038 ac-21804(20695) Volume 7 Vibrations Handbook for Helicopters

1954

37 PB 111521 Rotary Wing Aircraft Handbook and History Contract# W33-038 ac-21804(20695) Vol. 10 Stability and Control of Rotary Wing Aircraft

1954

38 PB 111288 Rotary Wing Aircraft Handbook and History Contract# W33-038 ac-21804(20695) Volume 13 Convertible Aircraft

1954

39 PB 111391 Rotary Wing Aircraft Handbook and History Contract# W33-038 ac-21804(20695) Volume 14 The Rotary Wing Industry

1954

40 ASD TR No. 61-660 Investigation of Flexible Rotor Systems – Results of Phase I & II Contract# AF 33(616)­7613

Sep 1961

41 WADC TR 55-408 Utilization of Helicopters as Army Fuel Tankers

Dec 1955

42 AHS Paper No. AHS-1 Helicopter Flight Research at NACA, Langley by Jack P. Reeder NACA

Dec 1951

43 AHS Paper Preliminary Development of a Trailing Rotor System by J.A. DeTore Bell

Nov 3-4 1965

44 AHS Paper No. 102 The helicopter Rotor at High Mach Speeds by W.H. Tanner & J.F. Van Wychhouse Bell and Patrick Cancro USAAMlabs and John McCloud, III NASA

May 10-12 1967

45 AHS Paper US Army Hueycobra Configuration and May 10-12 1967

90

Design Considerations by Charles M. Seibel Bell 46 AHS Paper No. 201 Status Report on Design Development

of the AH-56A Cheyenne by P.W. Theriault Lockheed-California

May 8-10 1968

47 AHS Paper No. 233 Experimental Flight Tests of the 300 MPH XH-51A Compound Helicopter by W.E. Spencer Lockheed-California

May 8-10 1968

48 AHS Paper No. 210 A Special Gas Turbine Cycle for the Compound Helicopter by J.B. Nichols United Technologies

May 8-10 1968

49 AHS Paper No. 216 Flight Investigation of the Wing-Rotor Lift-Sharing Characteristics of a Hingeless Rotor Compound Helicopter by Perry L. Deal & Julian L. Jenkins NASA Langley

May 8-10 1968

50 AHS Paper Flying Qualities Considerations in the Design and Development of the Hueycobra by C.L. Livingston & M.R. Murphy Bell

May 1968

51 Full Scale Wind Tunnel Test of a High Performance Helicopter Rotor Bell

Undated

52 SAE Paper No. 923C Aerodynamic Development of the OH-6A Helicopter for the Army by Kenneth B. Amer HTC

Oct 5-9 1964

53 AIAA Paper No. 93-4819 International Research in Rotorcraft Technologies by Alfred Gessow Univ. of Maryland

Dec 1-3 1993

54 Report No. R&M No. 1157 On the Horizontal Flight of a Helicopter

Mar 1928

55 Report No. F-IR-133-RE Helicopter Theory Interview with Dr. Kurt Hohenemser Concerning His Recent Contributions

Sep 1946

56 USAAVLABS TR 68-26 Preliminary Design Study of Convertible Fan/Shaft Engines Contract# DAAJ02-67-C­0070

Apr 1968

57 USAAVLABS TR 69-50 Exploratory Study of the Nature of Helicopter Rotor Blade Boundary Layers Contract# DAAJ02-67-C-0001

Jul 1969

58 NACA TN 3238 Review of Information on Induced Flow of a Lifting Rotor

Jun 1954

59 NACA TN 3690 Normal Component of Induced Velocity in the Vicinity of a Lifting Rotor with a Nonuniform Dick Loading

Apr 1956

60 NACA TN 3691 Analysis and Comparison with Theory of Flow-Field Measurements Near a Lifting Rotor in the Langley Full-Scale Tunnel

Apr 1956

61 NACA TN 3900 Investigation of Vertical Drag and Periodic Airloads Acting on Flat Panels in a Rotor

Dec 1956

91

Slipstream 62 NASA TN D-43 An Evaluation of Linearized Vortex

Theory as Applied to Single and Multiple Rotors Hovering in and Out of Ground Effect

Sep 1959

63 NASA TN D-112 Experimental Investigation of the Pressure Fluctuations on a Flat Plate and a Cylinder in the Slipstream of a Hovering Rotor

Sep 1959

64 Report No. FTD-MT-24-449-68 Aerodynamics of the MI­4 Helicopter

1967

65 Rotor Blueprints SE 3000 Undated 66 Helicopters – Miscellaneous Articles, Photos and

Brochures Various

ROTORS, HOT CYCLE ROTORS, STABILITY 36 1 Report No. FDM No. 267 Results of Data Flights on the

XHO3S-2 – Helicopter Stability Investigation Contract# AF33(616)-2773 Cornell

Apr 8 1957

2 Report No. FDM No. 271 The Determination of Helicopter Longitudinal Stability Derivatives from Phase II Flight Test Data Contract#AF33(616)-3772 Cornell

Jul 3 1957

3 Simulation of the Heavily Damped Mode (Short Period Mode) of the XHO3S-2 Helicopter on the EASE Analog Computer Using Linearized Equations of Motion Contract# AF33(616)-5361 Cornell

Oct 24 1957

4 Report No. FDM No. 280 Analyses of a 30 MPH Helicopter Flight Transient on the EASE Analog Computer Cornell

Feb 27 1958

5 Report No. FDM No. 292 A Preliminary Study of Helicopter Lateral Stability and Control Contract# AF33(616)-6049 Cornell

Jan 5 1959

6 Report No. FDM No. 294 Methods for Extracting Helicopter Lateral Stability Derivatives from Transient and Steady-State Flight Data Cornell

Apr 20 1959

7 Report No. R-217 A Review of Theoretical and Experimental Investigations of the Rotor Aerodynamic Problem Contract NONR 2811 (00) Boeing-Vertol

Oct 1960

8 Report No. PR-508 Advanced Flight Research Program Boeing-Vertol

1964

9 Report No. HTC-AD-65-15 Volume II Summary TR – Rotor/Wing Concept Study Contract# Nonr-4588(00) HTC

Sep 1965

10 Report No. HTC-AD-65-15 Volume I Appendixes A, B, C, D, E, and F to Summary TR – Rotor/Wing Concept Study Contract# Nonr-4588(00) HTC.

Sep 1965

11 Reporty No. HTC-AD-66-9 Rotor/Wing Series V Wind Tunnel Test – 1/15-Scale Transonic Model HTC

Sep 1966

92

12 Hot Cycle Rotor/Wing Concept HTC Feb 15 1968 13 PB 111632 Rotary Wing Aircraft Handbooks and History

Volume 8 Mechanical Design and Description Contract# W33038-ac-21804 (20695)

C.A. 1954

14 PB 111632 Rotary Wing Aircraft Handbooks and History Volume 11 Special Types of Rotary Wing Aircraft Contract# W33038-ac-21804 (20695)

C.A. 1954

15 Dynamic Antiresonant Vibration Isolator Kaman Undated 16 Report No. R-145 A Study of Aerodynamic Interaction

Between Lifting Rotors and Components in the Rotor Wash Contract# AF33(616)-2981 Kaman

Jul 23 1956

17 Report No. MTI-67RD627 Proposal for Hybrid Boost Bearing Development Sikorsky

Aug 11 1967

18 Report No. MTI 68RD670 Proposal for WPAFB – Hydrostatic Boost Spherical Ball Bearing for Helicopter Rotor Blade Joint Application, Design, Development and Testing Mechanical Technology

Apr 8 1968

19 Report No. HF 68-1 Injury Experience in Army Helicopter Accidents by Kenneth L. Mattox, CPT, MC

C.A. 1968

20 Report No. WAC 103 Proposal for a Preliminary Design Study of a Squad Carrying Combat Utility Transport Wilford

Apr 1970

21 TRW Systems Evaluation of Helicopter Evacuation Rescue Outfit (HERO) Presentation

Undated

22 Report No. 55McC103R Full Scale Investigation of Rotor Hub Fairing for a Sikorsky H-5 Rotor Hub Contract# AF 18(600)-176

Apr 1955

23 Helicopter Research & Development Conference Papers Bell

May 16-17 1961

24 Items of Interest and Suggestions for Research by Robert R. Lynn Bell

May 15 1968

25 Bibliography of Rotary Wing Aircraft C.A. 1940 26 Report No. 1-64 US Army Helicopter Accidents Involving

Fire C.A. 1964

27 TCREC TR 62-103 Hot Cycle Rotor Duct Closure Valve System Contract# DA 44-177-TC-832

Mar 1963

28 USAAVLABS TR 65-29 Aircraft Design XV-9A Hot Cycle Research Aircraft – Summary Report Contract# DA 44-177-AMC-877(T)

Aug 1965

29 USAAVLABS TR 65-68 Component Testing XV-9A Hot Cycle Research Aircraft – Summary Report Contract# DA 44-177-AMC-877(T)

Nov 1965

30 USAAVLABS TR 65-68 Ground and XV-9A Hot Cycle Research Aircraft – Summary Report Contract# DA 44­177-AMC-877(T)

Mar 1966

93

37 1 USAAVLABS TR 66-10 XV-9A Hot Cycle Research Aircraft – Summary Report Contract# DA 44-177-AMC­877(T)

Jun 1966

2 USAAVLABS TR 66-81 20-Hour Follow-On Flight Test Program, XV-9A Hot Cycle Research Aircraft Contract# DA 44-177-AMC-225(T)

Dec 1966

3 USAAVLABS TR 67-1 Preliminary Design of a Rotor System for a Hot Cycle Heavy-Lift Helicopter Contract# DA 44-177-AMC-225(T) Task II

Mar 1967

4 USAAVLABS TR 67-9A In-Flight Measurement of Rotor Blade Airloads, Bending Moments, Together with Rotor Shaft Loads and Fuselage Vibration, on a Tandem Rotor Helicopter – Volume I Instrumentation and In-Flight Recording System Contract DA 44-177-AMC-124(T)

May 1967

5 USAAVLABS TR 67-9B In-Flight Measurement of Rotor Blade Airloads, Bending Moments, Together with Rotor Shaft Loads and Fuselage Vibration, on a Tandem Rotor Helicopter – Volume II Calibrations and Instrumented Component Testing

May 1967

6 USAAVLABS TR 67-9C In-Flight Measurement of Rotor Blade Airloads, Bending Moments, Together with Rotor Shaft Loads and Fuselage Vibration, on a Tandem Rotor Helicopter – Volume III Data Processing and Analysis System

Nov 1967

7 USAAVLABS TR 67-9D In-Flight Measurement of Rotor Blade Airloads, Bending Moments, Together with Rotor Shaft Loads and Fuselage Vibration, on a Tandem Rotor Helicopter – Volume IV Summary and Evaluation of Results

Nov 1967

8 USAAVLABS TR 67-9E In-Flight Measurement of Rotor Blade Airloads, Bending Moments, Together with Rotor Shaft Loads and Fuselage Vibration, on a Tandem Rotor Helicopter – Volume V Investigation of Blade Stall Conditions

Apr 1968

SERIES VI: Convertiplane, Autogiro, Composite Research Vehicle and Stowed Rotor, 1923-1999

Box File Description Date

CONVERTIPLANE 38 1 Report 3371 The Development of a V-Tab Controlled

Floating Horizontal Tail For Rotary Wing Aircraft Contract # AF33(600)-22222 McDonnell

Jan 8 1954

2 Report 3379 Full Scale Rotor Tests of the AF Feb 4 1954

94

Convertiplane Model XV-1 NACA Wind Tunnel, Moffett Field, CA Contract# AF33(616)-487 McDonnell

3 Report 3359 Characteristics of the Model XV-1 Convertiplane in Airplane and Autogiro Flight Conditions NACA Wind Tunnel, Moffett Field, CA Contract# AF33(600)-9392 McDonnell

Nov 1 1954

4 Report 2347 Model 82 Preliminary Performance Data Report Contract# AF33(038)-28075 McDonnell

Nov 12 1951

5 Model 82 Mockup Design and Specifications McDonnell Oct 17 1956 6 Report 3652 Model XV-1 Performance Data Report

Contract# AF33(600)-9392 McDonnell Mar 1 1955

7 Data Book For Helicopter Phase Tests on Model 82 Convertiplane

Sep 25 1952

8 Report 3652 Model XV-1 Performance Data Report Contract# AF33(600)-9392 McDonnell

Mar 1 1955

9 Report 3377 Design, Fabrication and Test of a Tail System Design of Model 82 Convertiplane Contract# AF33(600)­22222 McDonnell

Dec 1 1953

10 Wind Tunnel Data Notebook 8/31 Scale Model 82 Convertiplane Massie Wind Tunnel Wright ADC

Dec. 1952-Jan. 1953

11 Report 1923 Aerodynamics Report Model 82 Dec 8 1950 12 Report 4459 XV-1 Drag Reduction Wind Tunnel Results

Contract# AF33(600)-9392 McDonnell Oct 31 1955

13 Wind Tunnel Investigation of the Aerodynamic Characteristics of an 8/31 Scale McDonnell Model 82 Convertiplane

Jan1954

14 Report 3386 Revision Dated 1 March 1956 Stability and Control Analysis of the McDonnell XV-1 Convertiplane Contract# AF33(600)-9392 McDonnell

Apr 6 1954

15 TN 54-2 Wind Tunnel Investigation of an 8/31 Scale McDonnell Model 82 Convertiplane in the Helicopter Flight Range

Jan1954

STOPPABLE/STOWED ROTOR/ CONVERTIPLANE

39 1 Ryan Stowed Rotor Aircraft Concept Article and drawings Jun 13 1968 2 LR 19755 VTOL Advanced Transport Aircraft Lockheed May 19 1966 3 Ryan VTOL Transport Potential 1975-1985 Undated 4 LTV The Promise of VTOL 1975-1985 Undated 5 Stoppable Rotor Aircraft Unidentified Appendices Undated 6 Hughes VTOL Briefing 1975-1985 Undated 7 Hughes Hot Cycle Rotor/Wing Undated 8 Performance of Advanced Heavy Lift Helicopters with Hot

Cycle Propulsion May 11-13 1966

9 Report SER-2600-23 Engineering Progress Report 23 Phase I of Development of Convertiplane Contract#

May 13 1953

95

AF33(038)-28076 Sikorsky 10 Report SER-2618 Aerodynamics Report S-57

Convertiplane Contract# AF33(038)-28076 Sikorsky Apr 21 1952

11 Report SER-2638 Substantiating Data for Standard Aircraft Characteristics and Performance Charts Contract# AF33(038)-28076 Sikorsky

Jul 2 1954

12 Report SER-2633 Detail Specification Model S-57 Convertiplane Contract# AF33(038)-28076 Sikorsky

Jun 2 1954

13 Report SER-2634 Preliminary Analysis of Airloads for Sikorsky S-57 Airplane Configuration Contract# AF33(038)-28076 Sikorsky

Jun 24 1954

14 Report SER-2639 Preliminary Load Report S-57 Convertiplane Contract# AF33(038)-28076 Sikorsky

Jul 2 1954

15 Sikorsky S-57 Convertiplane Engineering Drawings Contract# AF33(038)-28076 Sikorsky

1954

16 Report SER-2622 Estimated Weight and Performance Alternative Phase II Aircraft Contract# AF33(038)-28076 Sikorsky

Jun 20 1952

17 Report SER-2608 Detailed Calculation of Rotor-Wing Interference of S-57 for Vertical Climb and Hovering Contract# AF33(038)-28076 Sikorsky

Oct 11 1951

18 Report SER-2637 Preliminary Analytical Study of the Stability & Control of the Sikorsky S-57 Convertiplane Contract# AF33(038)-28076 Sikorsky

Jul 2 1954

19 Report SER_2609 Performance of the S-57 Powered by a T-38 Allison Turbo-Prop Powerplant Contract# AF33(038)-28076 Sikorsky

Oct 9 1951

20 Report SER-2636 Preliminary Group Weight and Balance Statement Contract# AF(33)-028076 Sikorsky

Jun 8 1954

21 Report SER-2642 History of a Non-Retractable Rotor & a Retractable Landing Gear for the Model S-57 Convertiplane Contract# AF33(038)-28076 Sikorsky

Jul 8 1954

22 HTC-AD 66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 2 – Performance Data HTC

May 1966

23 Report SER-50631 (Volume II) Stoppable Rotor Study – Wind Tunnel Plan Contract# F33615-69-C-1579 Sikorsky

Oct 15 1969

24 Wind Tunnel Investigations of a High Speed Stowed Rotor Aircraft

1968

25 Code Ident. No 81205 Stowed Rotor Aircraft Transport Parametric Study by Boeing-Vertol

1965

26 USAAVLABS TR 69-7 The Aerodynamic and Aeroelastic Characteristics of a Full-Scale Rotor Blade Stopped in Flight Contract# DA 44-177-AMC-366(T)

Apr 1969

27 Report R-598 Kaman Aircraft Model K-120 Composite Aircraft Kaman

Jul 30 1965 Rev Feb 7 1966

28 WSDS 68-18 Preliminary Weight and Performance May 1968

96

Analysis of AFFDL Transition Wing, Stopped Rotor Aircraft Concept

29 HTC-AD 65-15 Volume II Appendixes A, B, C, D, E, and F to Summary TR Rotor/Wing Concept Study Contract# Nonr-4588(00) HTC

Sep 1965

30 HTC-AD 65-15 Volume I Summary TR Rotor/Wing Concept Study HTC

Sep 1965

31 HTC-AD 66-1 TR Hot Cycle Rotor/Wing Composite Research Aircraft Section 3 Propulsion System HTC

May 1966

STOWED ROTOR (LOCKHEED COMPOSITE RESEARCH VEHICLE)

40 1 LR 19539 Composite Research Aircraft Lockheed May 1966 2 LR 19534 Review Draft Preliminary Design Study and

Proposal For Full Scale Follow-On Program Volume 1 – Technical M-Statement of Work For Follow On Phase Contract# DA-44-177-AMC-372(T) Lockheed

May 1966

3 Report 16661 Wind Tunnel Investigation of a Hybrid Helicopter Dynamic Model Lockheed

Mar 25 1963

4 Report 17865 Experimental Investigation of Rotor Model Stop/Start in Forward Flight Lockheed

Jun 2 1964

5 USAAVLABS TR 68-40 Stopped-Stowed Rotor Composite Research Aircraft

Jan 1969

6 LR 19538 Trade-Off Analysis for Stowed Rotor Concept Lockheed

May 1966

7 LR 19535 Review Draft Preliminary Design Study and Proposal for Full-Scale Follow-On Program Volume 1 – Technical N-Plan of Performance for Full Scale Follow-On Contract# DA-44-177-AMC-372(T) Lockheed

May 1966

8 LR 21793 Selected Bibliography Lockheed Undated 9 LR 19522 Review Draft Preliminary Design Study and

Proposal For Full-Scale Follow-On Program Volume 1­Technical A- Design Concept Contract# DA-44-177­AMC-372(T) Lockheed

May 1966

10 LR 19523 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1­Technical B-Performance Data Contract# DA 44-177­AMC-372(T) Lockheed

May 1966

11 LR 19540 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume II Management Contract# DA 44-177-AMC-372(T) Lockheed

May 1966

12 LR 19541 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume III

May 1966

97

Cost Contract# DA-44-177-AMC-372(T) Lockheed 13 LR 19524 Review Draft Preliminary Design Study and

Proposal For Full-Scale Follow-On Program Volume 1­Technical C Propulsion Data Contract# DA 44-177-AMC­372(T) Lockheed

May 1966

14 LR 19525 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1­Technical D-Weight and Balance Contract# DA 44-177­AMC-273(T) Lockheed

May 1966

15 LR 19526 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1­Technical E-Stability, Control and Flying Qualities Contract# DA 44-177-AMC-372(T) Lockheed

May 1966

16 LR 19528 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1­Technical G-Electrical, Hydraulic and Mechanical Systems Contract# DA 44-177-AMC-372(T) Lockheed

May 1966

17 LR 19536 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1­Technical O-Test Plans for Full-Scale Follow-On Contract# DA 44-177-AMC-372(T) Lockheed

May 1966

18 LR 19537 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1­Technical P-Draft Specification Contract# DA 44-177­AMC-372(T) Lockheed

May 1966

19 LR 19529 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1­Technical H-Emergency Systems and Procedures Contract# DA 44-177-AMC-372(T) Lockheed

May 1966

20 LR 19530 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1­Technical I-Cockpit Arrangement Contract# DA 44-177­AMC-372(T) Lockheed

May 1966

21 LR 19531 Review Draft Preliminary Design Study and Proposal For Full-Scale Follow-On Program Volume 1­Technical J-Drawings Contract# DA 44-177-AMC-372(T)

May 1966

CONVERTIPLANE / COMPOSITE RESEARCH AIRCRAFT

41 1 RDM Convertiplane and Engine Jun 1951 2 Report 2R90-10 Quarterly Report Contract# AF33(616)­

3647 Transcendental Aircraft Corp. Task 449L Project R­56-662-TC

Sep 15 1956

3 Bell XV-3 Articles, Pictures and Summary Feb 10 1955 4 Report 301-199-001 V/STOL Tilt Rotor Research Aircraft

Volume 1 Performance and Noise Analysis Contract# Jan 1973

98

NAS2-7260 Bell 5 Report 200-094-233 Determination of Stability Derivatives

for Two Center of Gravity Locations from Wind Tunnel Tests of Bell Model 200 (XH-33) Bell Convertiplane

May 23 1955

6 Report200-099-703 Dynamic Stability Analysis for the XV-3 Convertiplane Bell

Sep 1 1955

7 Bell Helicopter Brochure Model 301 Tilt Rotor Aircraft Bell

Dec 1973

8 Report 200-102-100 Aerodynamic and Performance Data for the XV-3 Convertiplane Bell

Mar 11 1954

9 Report 200-094-232 Wind Tunnel Investigation of Airplane Flight Characteristics of the Bell Model 200 Convertiplane Volume 1 Analysis and Discussion of Results Bell

Oct 12 1953

10 Report 200-094-238 Wind Tunnel Investigation of Lateral – Directional Stability of the XV-3 Convertiplane Bell

Feb 1 1955

11 Bell XV-3 Convertiplane Photos and Articles for Contract# AF33(600) 20777

1954

12 Report AR-B103 Preliminary Stability and Control Analysis of the Model B Convertiplane Convertawings, Inc.

Dec 7 1950

13 Quarterly Progress Report (15 Sept. 56 – 15 Dec. 56) Transcendental Aircraft Corp. Task No. 449L, Project No. R-56-662-TC Contract# AF33(616)-3647

Jan 15 1957

14 Transcendental Aircraft Corp. Interim Progress Report Contract# AF33(616)-3647

Oct 31 1956

15 Report D26-099-101 Composite Research Aircraft Design Study – Design Concept- Contract# DA 44-177-AMC­373(T) Bell

May 1966

16 Report D26-099-102 Composite Research Aircraft Design Study – Performance Data- Contract# DA 44-177-AMC­373(T) Bell

Undated (probably May 1966)

17 Report D26-099-103 Composite Research Aircraft Design Study – Stability, Control and Flying Qualities - Contract# DA 44-177-AMC-373(T) Bell

May 1966

18 Report D26-099-105 Composite Research Aircraft Design Study – Propulsion Data- Contract# DA 44-177-AMC­373(T)

May 1966

19 Report D26-099-107 Composite Research Aircraft Design Study – Emergency Systems and Procedures- Contract# DA 44-177-AMC-373(T) Bell

May 1966

20 Report D26-099-111 Composite Research Aircraft Design Study – Detail Specification (Draft) - Contract# DA 44­177-AMC-373(T) Bell

May 1966

21 Report D26-266-101 Composite Research Aircraft Design May 1966

99

Study – Results of Model Test- Contract# DA 44-177­AMC-373(T) Bell

22 Tilt Rotor Composite Aircraft Articles May 1971 23 Bell Helicopter Proprotor VTOL Technology Program Mar 16 1970 24 Bell TiltRotor Photos and Vugraphs 1966 25 The Rheem-Platt Vertical Take-Off Airplane Aerodynamic

Analysis Sep 16 1947

26 Northrup Norair Division Article – About the Application of Low Drag Boundary Layer Suction to Tilt Rotor Propeller Blades During Cruising

Apr 1967

27 Bell Article – An Analysis of Low-Disc-Loading VTOL Aircraft Types

Jan 10-13 1966

STOPPABLE/STOWED ROTOR/ CONVERTIPLANE 42 1 Report SER-50621 Stoppable Rotor Study Phase I – Final

Report Sikorsky Oct 1 1969

2 AFFDL-TR-71-62 Volume 1 Design Studies and Model Tests of the Stowed Tilt Rotor Concept

Jul 1971

3 AFFDL-TR-72-81 Summary of Design Studies and Results of Model Tests of the Folding-Prorotor Aircraft Concept

Jul 1972

4 USAAVLABS TN 70-28 Convertible Fan/Shaft Engine Variable Fan Geometry Investigation Contract# DAAJO2­69-C-0002

Apr 1970

5 Summary of Mission Design Studies for Folding Tilt Rotor Aircraft Boeing-Vertol

Jun 3 1969

6 Horizontal/Stoppable Rotor Articles and Concept Photos 1969 7 AHS 27th Annual National V/STOL Forum– Horizontal

Stoppable Rotor Conversion by George A. Watts & James C. Biggers Lockheed & NASA Ames

May 1971

8 Report D270-099-001 Design Studies of Folding-Prorotor VTOL Aircraft Bell

Oct 1969

9 R&D Interim Report of Phase I – Design Studies and Model tests of the Stowed Tilt Rotor Concept – Volume I. Parametric Design Studies

Sep 1969

10 Report 2D-3210-1 Summary Report Helicopter Model 2D Gyrodyne

Jul 1953

11 Report 2C-3336-2 Performance Demonstration Report Model 2C Contract# NOas 51-1217-f Gyrodyne.

Sep 26 1952

12 Report 2C-3336-3 Flying Qualities Demonstration Report Model 2C Contract# NOas 51-1217-f Gyrodyne

Oct 15 1952

13 Report 2C-3336-5 Spoiler Evaluation Report Model 2C Contract# NOas 51-1217-f Gyrodyne

Dec 12 1952

14 Report 2C-3336-6 Supplementary Flying Qualities Report Model 2C Contract# NOas 51-1217-f Gyrodyne.

Dec 26 1952

15 Report 2C-3336-7 Directional Control Tests with Blade Tip Air Brakes Contract# NOas 51-1217-f Gyrodyne

Apr 14 1953

100

16 Report 2C-3336-8 Summary Report Model 2C Flight test Results Contract# NOas 51-1217-f Gyrodyne

May 11 1953

17 Report 102X90-4 An Investigation of the Handling Qualities of a Tandem Rotor Helicopter (H-21) Equipped with a Gyroscopic Stabilizing System Contract# NOas 56­796-c Kellett

Aug 1 1958

18 US Army TRC Preliminary Flight Test Data UH-1B High Performance Helicopter with Auxiliary Propulsion

Feb 1964

19 US Army TRC Preliminary Flight Test Data XH-51A Rigid Rotor High Speed Flight Program Interim Report No. 4

Oct 1964

20 Operational History and Experience with Boeing Helicopters by Howard N. Stuverude

Nov 14-16 1967

21 NASA TN D-4195 A Numerical Method for Studying the Transient Blade Motions of a Rotor with Flapping and Lead-Lag Degrees of Freedom

Oct 1967

22 Report FT-13R-66 Monitor of the Development of Helicopter and VTOL Research Programs; Third Interim Report

Dec 13-17 1965

23 Development of a Piloted, Real Time, Hybrid Simulation of the X-22A V/STOL Aircraft by William G. Cockayne Bell

Undated

24 Report 2127-950006 Flight Test Summary Report X-22 Aircraft No. 1 (BuNo 151520)

Sep 19 1966

43 1 KELLETT DRAWINGS

STOPPABLE & STOWED ROTOR 44 1 Stoppable Rotor Program – Briefings and Slides Nov 1969

2 Stoppable Rotor Program – Reports and Analysis with Handwritten Notes

C.A. 1969

3 Stoppable Rotor Program – Phase I Briefing Contract#F33615-69-C-1578 (6 sections and photo) Bell

Oct 30 1969

4 Folding Proprotor Program Briefing Contract# NAS 2­5461 Bell

Jan 15 1970

5 Proprotor Landing Gear Memo Bell Jan 7 1970 6 Design Criteria for Folding Tilt Rotor Aircraft Contract#

F-33625-69-C-1577 Boeing Vertol Oct 1969

7 Report DRC-268 Downwash Environment for the Boeing Model 160 V/STOL Aircraft Dynasciences

Jan 1968

8 Stoppable Rotor Program – 1) Feb 1968 Calender; 2) VTOL Aircraft Chart; 3) Operational and Summary Evaluation Matrixes; 4) Lindenbaum Notebook

Feb 1968

9 Proposal For Analytical and Experimental Study of a New VTOL Concept VRC.

Jul 5 1960

10 Convertible Aircraft – Article, Sketches and Photo Jan 1953

101

11 Wing Rotor Configuration Research Plan Oct 23 1967 12 Stoppable Rotor Program – Concept Assessment Report Jan 2 1968 13 Stoppable Rotor Program – NAA Meeting Report Jan 22 1968 14 Report D-213-100000-2 R&D Interim Report of Phase I –

Design Studies and Model Tests of the Stowed Tilt Rotor Concept Volume III Appendixes Contract#F33615-69-C­1577 Boeing

Sep 1969

15 Report D-213-100000-3 R&D Interim Report of Phase I – Design Studies and Model Tests of the Stowed Tilt Rotor Concept Volume II Component Design Studies Contract#F33615-69-C-1577 Boeing

Sep 1969

16 Report D-213-100001-1 R&D Interim Report of Phase II – Design Studies and Model Tests of the Stowed Tilt Rotor Concept Contract#F33615-69-C-1577 Boeing

Sep 1969

17 The Helijet Lateral Twin Folding Rotor V/STOL Aircraft Boeing Vertol

Feb 15 1968

STOWED/STOPPABLE ROTOR 45 1 Report SEP 6229 Stowed Rotor V/STOL Program

Planning Proposal SPB 64-AF9063-US Sikorsky Mar 23 1964

2 Report SEP-6260 Stowed Rotor V/STOL Flight Program Proposal SPB 64-AF1854-US Sikorsky

Oct 30 1964

3 Circulation Control Rotor Program for Advanced Technology Navy/Marine Helicopters

Undated

4 Stowed Rotor Helicopter Program Blueprint and Partial Document Sikorsky

C.A. 1964

5 Stoppable Rotor – Miscellaneous C.A. 1964-1965 6 Stoppable Rotor – Study Plan & Briefings Oct 10 1967 7 NASA Literature Search No. 5331 Stoppable Rotor

Aircraft Dec 1 1967

8 IAS Paper No. 62-62 The Hot Cycle Jet Rotor for Economical VTOL Aircraft by Malcolm Harned HTC

Jan 22-24 1962

9 Bell Stoppable Rotor Nov 3-4 1965 10 Stowable Rotor V/STOL Sikorsky Jan 20 1964 11 Application of Circulation Control Rotor Technology to a

Stopped Rotor Aircraft Design by Robert M. Williams Sep 22-24 1975

12 Proposal for the Development of a Vertical Take-Off and Landing Aircraft Prewitt Plastics Co.

Apr 4 1961

13 Report D2064-953001 Tri Service VTOL Transport – Proposal Summary Vol I Part I Bell/Lockheed

Apr 1961

14 Vertol Stoppable Rotor C.A. 1967 15 Berguet 941 VTOL Transport – Detail Specification

Summary Report for Tri-Service VTOL Prototype Aircraft Apr 9 1961

16 Sikorsky Stowed Rotor – Blueprints and Sketches C.A. 1964 17 Conversion of Berguet’s STOLs to VTOLs by Harlan D.

Fowler with Additional Calculations Oct 10 1960

102

18 Report ARD-211 VTOL Amphibious Assault Transport Systems 1962-1967 Phase III Summary report Hiller

Apr 15 1959

19 59RDZ-34581 Grumman Report to the Perkins Committee 1959 20 Stoppable Rotor Program – Pictures, Negatives and

Overhead Projection Slides Various

21 The Future of Vertical Take-Off and Landing Aircraft by Philip L. Michel Sikorsky

Oct 1967

22 Research and Development by Philip L. Michel Sikorsky Jan 1963 23 Stoppable Rotor Concepts and Descriptions Used in

CARA Evaluation Undated

24 Photos Undated 25 V/STOL Photographs

(See also Location 50, File 3 for drawings/prints of various V/STOL Aircraft & Helicopters – mounted on cardboard)

Undated

26 Legal Aspects of Planning for Urban Heliports by L. Welch Pogue & George C. Neal Virginia Law Review Vol. 46, No. 1

1960

27 NASA TN D-814 Nomographic Solution of the Momentum Equation for VTOL-STOL Aircraft

Apr 1961

28 NASA TN D-5819 Theoretical Study of Conditions Limiting V/STOL Testing in Wind Tunnels with Solid Floors

Jun 1970

29 AERO Report 954 Comparison of Experimental and Theoretical Design Parameters of a 6 Inch Diameter Annular Jet Model with a Jet Angle of -45o Hovering in Proximity to the Ground: and Experimental Results for Forward Flight at Zero Angle of Attack

May 1959

30 NACA RM L53A09 Langley Full Scale Tunnel Tests of the Custer Channel Wing Airplane (Cover missing)

Undated

31 Report 16-A-3 The Ring Tail as a Stabilizer and Control Device Piasecki

Aug 26 1960

32 Report 2-Y-4 Ring-Wing V/STOL Logistics Aircraft Piasecki

Feb 25 1960

33 V/STOL Logistic Aircraft Blueprints by Harlan D. Fowler C. A. 1960

34 SAE 266G Mass Transportation by High-Speed VTOL by H.V. Borst & J.M. Mergen Curtiss

Jan 9-13 1961

35 V/STOL Logistics Aircraft ARDC SR. No. 175 by Harlan D. Fowler

Jan 28 1960

36 Report 60-6 New Transport Aircraft 1965-1970 Time period Hiller

Feb 1960

37 Report 59RDZ-15303 Program Planning Report Pre-Phase 1 Part 1 and Part 2 – Development Program VTOL Supersonic Aircraft Contract# AF33(600)-39722 AVRO

Jun 1959

38 Report ZP-258 Preliminary Study Comparative Characteristics of Tilt-Wing, Ducted Propeller & G.E. Lift-

May 20 1959

103

Fan Military transport Type Aircraft With Combined VTOL & STOL Capability Convair

39 AIAA Paper 69-198 The Outlook for Future Commercial VTOL Transportation by Robert W. Simpson MIT

Feb 17-19 1969

40 Report D8-2357-8 Light Tactical Transport Aircraft System (LTTAS) Final Report Volume VIII Boeing

Jul 1969

41 SAE 650807 V/STOL Transport Aircraft for Air Cargo Operations by G.B. Pearson LTV

Oct 4-8 1965

SAE 660335 Vertical Flight in Common Carrier Transportation by Robert L. Cummings NYAirways

Apr 25-28 1966

42 SAE 700809 Planning the Evolution of V/STOL Powerplants by A.G. Newton & S.C. Miller Rolls-Royce Ltd.

Oct 5-9 1970

43 AIAA Paper 71-1015 STOL, VTOL, and V/STOL – Where Do They Fit In?

Oct 25-28 1971

44 NASC Report 3032-72-02 A Suggested Way for Comparing VTOL Configurations

May 1972

45 FDV 10-7-34 V/STOL Low Disc Loading Technology Oct 11 1967 46 Survey Paper on the Application of Technology to the

Flight Mechanics of Aircraft Development by Lawrence P. Green, Clem C. Weissman & Jack D. Brewer

Sep 13 1967

47 AIAA Paper 67-711 Study of Aircraft in Short-Haul Transportation Systems for 1985 by Donald W. Hayward Boeing

Oct 23-27 1967

48 Study of Aircraft in Short-Haul Transportation Systems Contract# NAS2-3862

1967

49 VTOL Aircraft Concepts and Development by B. Lindenbaum

Apr 8 1965

50 Observations on Subsonic V/STOL Aircraft Designs for USAF by Bernard Lindenbaum

Jun 30 1960

51 SOR-210 Mar 1964 52 AGARD Flight Mechanics Panel Symposium on “Military

Applications of V/STOL Aircraft” TRIP REPORT by Major Robert M. Bowman USAF

Dec 27 1972

53 SAWE Paper 842 A Merit Factor Suitable for Evaluation of a Variety of Aircraft Types and Missions by Gavid F. Gebhard Grumman

May 4-6 1970

54 Evaluation of V/STOL Vehicles for Flight Control Research Flight Testing USAF Flight Dynamics Lab

Aug 1965

55 The Economics of VTOL Systems Apr 29 1966 56 FSTC-HT-23-1062-70 Battle Zone Transports of the

Future (Germany) Jan 1970

57 VTOL Negatives and Articles 1967 58 Sikorsky Stowed Rotor Fighter Undated 59 Stoppable Rotor – Photos, Slides, Miscellaneous Undated

104

XF5U AIRCRAFT 46 1 XF5U-1 Illustrated Assembly Breakdown Undated

2 References for Information on Sikorsky V-173 and Vought XF5U-1 Aircraft

Various

3 The Development of the Chance Vought Model XF5U-1 Airplane Contract NOa(s)270

May 11 1948

4 Air Classics Magazine with Article on ZF5U-1 (pg 16) Aug 1975 5 Recommended Circular Wing Design Study Jan 10 1973 6 Articles Concerning Circular Wing Model Aircraft Various 7 XF5U-1 Pilot’s Handbook Undated 8 Log of Flights & Pilot’s Daily Flight Progress(unreadable) Undated 9 NACA Research Memorandum RM L9C29 Preliminary

Full-Scale Investigation of a 1/3 Scale Model of a Convertible-Type Airplane

Jun 7 1949

10 Report 4876 (unreadable) Undated 11 XF5U-1 Handwritten notes and memos 1972-1973 12 Report 5711 (unreadable) Mar 28 1945 13 AFFDL TM 72-3-PTB Conceptual Study of a Low Aspect

Ratio Wing Design for a Close Air Support Mission Nov 2 1972

14 NACA Research Memorandum RM L9C24 Static Longitudinal Stability and Control of a Convertible-Type Airplane as Affected by Articulated and Rigid-Propeller Operation

Nov 7 1949

15 XF5U-1 Photos Undated 16 XF5U-1 Articles and Diagrams 1972

AUTOGIRO/CONVERTIPLANE 47 1 Rotorcraft/Contractor/Contract# Cross Reference Aug 28 1951

2 Roadable Autogiro by B. Lindenbaum and Supporting Documents

Nov 1971

3 Illustrations for Roadable Autogiro Report Nov 1971 4 Elementary Aerodynamics of Compound Rotorcraft by

W.Z. Stepniewski & R. Bumstead Piasecki Undated

5 Report No. SER-2000 Determination of Parasite Drag from Wind Tunnel and Flight Test Data Sikorsky

Sep 9 1949

6 Turbine Powered Aircraft (Alouette II) General description Advanced Copy Republic Aviation Corp.

Mar 2 1959

7 Rotodyne Brochure Kaman Aircraft Undated 8 Compound Helicopters – Clippings and Photos Various 9 Sikorsky S-65-200 Compound V/STOL Brochure Undated 10 Sikorsky S-61 Brochure Undated 11 Sikorsky H-39 Experimental Brochure Undated 12 Report No. 1921 Model Specification for McDonnell

Model 82 Convertiplane Stripped Version Contract# Dec 8 1950

105

AF33(600)-9392 13 Piasecki Aircraft Corp. Brochure Undated 14 Towing with the Vertol 44 Brochure Undated 15 The Case for the Tandem Helicpoter by Z.M. Ciokosz &

W.Z. Stepniewski Piasecki Helicopter Corp. Dec 17 1954

16 Report No. 255-X-3 Proposal for Air to Air Launch and Retrieval System Piasecki Aircraft Corp.

May 13 1972

17 Helicopter Photos (Early Years) Undated 18 AIAA 1999-01-5644 Advanced Flying Automobile LS1

Engine by Mike Czajkowski Oct 19-21 1999

19 AIAA 1999-01-5625 Starcar on the Road by Steven C. Crow

Oct 19-21 1999

20 Roadable Aircraft From Wheels to Wings by Palmer Stiles Copyrighted

1994

21 Report No. R-550 HH-43F “Huskie” Brochure Aug 1964 22 AN 01-260HBA-1 Flight Handbook for Navy Model

HOK-1 Helicopters Apr 15 1955 Rev. Feb 1 1956

23 Report No. 47-980-004 Model 47 tail Rotor Test Technical Data Bell

Aug 13 1947

24 Sikorsky Current Production Models Brochure Mar 1971 25 Report No. SD-466-2 Detail Specification for Model

HO4S-2 Helicopter Class HO Single Engine Contract NOas 51-220

Feb 13 1951

26 ER No. 62-73 Model Ten99A as a Missile Site Support Helicopter Hiller Aircraft Corp.

Aug 1962

27 AFFTC-TN-60-8 Performance Evaluation of the Djinn Helicopter

Feb 12 1960

28 Hiller Camel (Civil Version) Brochure Undated 29 WADC TR 55-437 Part II An Investigation of the

Handling Qualities of a Sikorsky H-19 Helicopter Equipped with Various Mechanical Stabilizers Part II. Flight Test Evaluation of the Optimum Stabilization System

Mar 1959

30 WADC TR 55-438 Part II The Determination of Helicopter Longitudinal Stability Derivatives from Flight Test Data Part II. Analyses of Flight Data and Extraction of Basic Stability Derivatives

Mar 1959

31 WADC TR 55-438 Part III The Determination of Helicopter Longitudinal Stability Derivatives from Flight Test Data Part III. An Analog Computer Study of Flight Measured Longitudinally Transient Motion of a Single Rotor Helicopter

Sep 1959

32 WADC TR 57-583 Part III Helicopter Configuration and Propulsion Systems Study Part III. Aerodynamic Analysis

Nov 1957

106

33 WADC TR 57-583 Part IV Helicopter Configuration and Propulsion Systems Study Part IV. Analytical Procedure for Predicting Rotor Weight

Nov 1957

34 Report No. 48-980-003 YH-12B High Tip Speed Flight Test Evaluation Contract# AF 33(600)-6473

Nov 17 1954

35 Report No. SER-126 Flight Test measurements of the Stresses and Relative Motions of the Main Rotor Blades Contract# DA W535 ac-2514 and ac-29845 Sikorsky

Dec 15 1944

36 WADC TR 55-438 Part I The Determination of Helicopter Longitudinal Stability Derivatives from Flight Test Data Part I. Development of Flight Test Instrumentation, Techniques and Analysis Methods

Feb 1958

37 Report No. ARD 134 Quick Starting of Ramjet Powered Helicopter Rotor Hiller Helicopters

Feb 20 1957

38 Report No. SER-538 Performance – Tail Rotor Sikorsky Oct 9 1944 39 ER No. J1-040-1 Discussion of Proposal and General

Description of Model 38 Jet Powered Helicopter McDonnell

Feb 13 1946

40 Report No. 1572 Progress Report No. 41 – Month of January 1950 – Rotor-Helicopter, Jet-Propelled, with Flyable test stand Contract# AF33(038)-9845 McDonnell

Feb 15 1950

41 Report No. 1576 Preliminary Design Data – High Tip Speed Ram Jet Rotor Contract# AF33(038)-9845 McDonnell

Feb 22 1950

42 Report No. ATD-TTH-Y24 The Gates Twinjet Helicopter Technical Information Bulletin Gates Learjet

Jul 1 1970

43 USAAMRDL TR 72-44 Fan-In-Fin Antitorque Concept Study Contract# DAAJ02-71-C-0060

Jul 1972

44 Huey Tug Brochure Bell Undated 45 ER No. 60-5 A Parametric Study of the USArmy New

Light Observation Aircraft 1965-1970 Time Frame. Hiller Feb 1960

46 Report No. 46-947-001 Proposed Model Specification for Single Engine-Two Bladed Helicopter Bell

Aug 10 1945 Rev Sep 10 1945

47 Report No. 47-947-015 Specification for Helicopter – Two Place – Single Engine – Two Bladed Contract# AF 33(038)15940

Sep 15 1951

48 Miscellaneous Papers and Articles Various

CONVERTIPLANE/COMPOUND HELICOPTER 48 1 Report No. 16-X-12 Model 16H Helicopter Overview

Piasecki C.A. 1962

2 Report 16-X-12D Military Applications of 16H V/STOL Aircraft Piasecki

May 28 1962

3 Report 16-X-12DE Piasecki 16H Compound V/STOL Jun 15 1962

107

Aircraft Piasecki. 4 Report 16-X-15a Fiscal Proposal 16H-1 Test and

Evaluation Program Piasecki May 12 1962

5 Report 16-X-17 Cost Effectiveness and Comparisons Piasecki

May 1 1962

6 Report 16-X-18 Proposal For Test Evaluation of a Compound Helicopter Configuration Piasecki

May 15 1962

7 Report 16-X-13 Proposal For Test Evaluation of a Compound Helicopter Configuration Piasecki

Mar 14 1962

8 Report SER-2551 Long Range Helicopter Method of Analysis – Compound Helicopter Configuration Sikorsky

Feb 18 1955

9 Report SER-2555 Long Range Helicopter Design Study Contract# AF33(616)-2628 Sikorsky

May 23 1955

10 Report SER-2556 Summary Report Long Range Helicopter Method of Analysis – Pure Helicopter Configuration Contract# AF33(616)-2628 Sikorsky

May 27 1955

11 Report SER-611344 Final Report NH-3A (Sikorsky S-61F) Flight Test Program Contract# Now-64-0528-f

Mar 20 1969

12 FSTC-HT-23-1554-72 New Technology of Fast Italian Helicopters

Mar 14 1973

13 USAAVLABS TR 71-2 High Mach Number/High Advance Ratio Flight Test Program with the High-Performance UH-1 Compound Helicopter Contract# DA 44-177-AMC-364(T)

Feb 1971

14 USAAVLABS TR 67-18 Rotor Blade Loads, Blade Motion, and Stress Caused by Transient Inputs of Shaft Torque as Related to Stoppable Rotor Operations Contract# DA-44-177-AMC-77(T)

May 1967

15 USAAVLABS TR 67-58 16H-1A Flight Test Research Program Contract# DA-44-177-AMC-154(T)

Aug 1968

16 WADC TR 53-125 Wind-Tunnel Investigation to Determine the Critical Advance Ratio of the 8/31-Scale McDonnell Model 82 Convertiplane Rotor

Apr 1953

17 WCLS TN 54-29 Tests on a 1/6-Scale Jacobs 104 Convertiplane Model in WADC Five-Foot Wind Tunnel

Apr 1954

18 The Generalized Actuator Disk by G.R. Hough & D.E. Ordway

Mar 5-6 1964

19 The Promise of Compounding by Jan M. Drees & Robert R. Lynn Bell

Jan 13-16 1966

20 Report No. 3447 Airplane Tow of the XV-1 for Long Range Rescue Missions Contract# AF33(600)-9392

Feb 24 1954

21 Tables for Computing the Instantaneous Velocities Induced at the Blade Axes of a Lifting Rotor in Forward Flight by the Skewed Wake Helical Wake Vortices and a Method for Calculating the Resultant Blade Air Loads Contract# Nonr 991(05) Georgia Tech

Jun 1962

108

22 AFFTC-TR-56-35 ARDC XV-1 Phase II Flight Evaluation Feb 1957 23 TR 107-1 Programs for Machine Computation of Rotor

Blade Downwash Contract# Now 62-0100-d MIT Aug 1964

24 Report No. R 242 Fundamentals of Helicopter Stability and Control Contract# Now 60-0469-f Boeing Vertol

Feb 1961

25 Report No. 8011-099-002 The Weight of Very Large Rotors for Nuclear Powered Helicopters Bell

Apr 23 1959

26 Report No. BB-1187-H-1 Improvement of Ferrying Range of Army Helicopters Contact# DA-44-177-TC-441 Cornell

Jan 1958

27 Report No. R-240 General Management Proposal for a Medium Transport Helicopter 58MCXS-13805

Aug 15 1958

28 Army Study Requirement 3-60 The Kaman Rotodyne Undated 29 Report 104-A-01 Performance Analysis of Jacobs 104

Helicopter Undated

30 Report D-114 A Review of the Convertiplane Development Program Jacobs Aircraft Engine Co.

Apr 22 1955

31 Report 3294 McDonnell V-1 Convertiplane Contract# AF33(038)-28075

Oct 26 1953

32 Report No. 1901 McDonnell Model 78 Assault Transport Helicopter

Dec 20 1950

33 Report No. 6248 Model 113P Medium Transport Compound Helicopter 58MCXS- 13806

Aug 18 1958

34 Report No. 3371 The Development of a V-Tab Controlled Floating Horizontal Tail for Rotary-Fixed Wing Aircraft Contract# AF33(600)-22222

Jan 8 1954

35 Report No. 2230 An Estimate of Propeller Effects on Static Longitudinal Stability of Model 82 Convertiplane Contract# AF33(038)-28075

Aug 21 1951

36 Miscellaneous Articles Various

AUTOGIROS – PRE WWII 49 1 Autogiros, Pre-World War II – Photos and Clippings Pre 1941

2 Aurogyio Photos Various

3 R&M No. 885 Some Experiments on Airscrews at Zero Torque, with Applications to a Helicopter Descending with Engine “Off”, and to the Design of Windmills by C.N.H. Lock

Sep 1923

4 R&M No. 1162 A Summary of the Experimental and Theoretical Investigations of the Characteristics of an Autogiro by H. Glauett & C.N.H. Lock

Apr 1928

5 Autogiro – Articles Various 6 Model 18-A Gyroplane – Weldon F. Stump and Co. Undated 7 Report No. ER-200 & ER-201 Report on Tests to

Determine Friction in Jump-Off Mechanism(ER200) and Feb 26 1938 Mar 10 1938

109

PA-36(ER201) Autogiro Co. of America 8 Report No. ER-130.4 Possibilities of “Jump-Off” Giro

Utilizing Optimum Blade Incidence Angles Kellett Feb 1935

9 Hafner AR-3 Gyroplane 1937 10 Cievra C-30 Autogiro 1928 11 Air Ministry reports and Memoranda Concerning

Autogiros No. 1108(Aug 1926); No. 1111(Nov 1926); No. 1127(Mar 1927): No. 1131(Jul 1927); No. 239.Vol.XXXIV(Nov 1930)

1926-1930

12 The Direct Control Autogiro Autogiro Co. of America Undated 13 Journal of The Franklin Institute Feb 1939

Mar 1939 14 The Aircraft Yearbook by Aeronautical Chamber of

Commerce – Volume 16, 17 and 24 1934, 1935, 1942

15 The Autogiro – Second Complete Authoritative Presentation Autogiro Co. of America

Undated

16 Copy of Brochure “What the Autogiro Co. of America Offers”

Undated

17 NACA No. 205 The Hafner A.R. III Gyroplane (British) Apr 1937 18 Testimony Before the Committee on Military Affairs of the

House of Representatives by Harold F. Pitcairn Autogiro Co. of America

Apr 26 1938

19 Recent Air Corps Developments in Rotating Wing Aircraft by H.F. Gregory

Jan 29 1941

20 Comparison of Flying machines by Juan de la Cievra Feb 1934 21 Kellett YG-1 Autogiro 1935 22 Kellett YG-1/KD-1 Autogiro Correspondence Various 23 Kellett XO-60 Autogiro 1943 24 TCTC 2175 Meeting 112 Military Characteristics for

Airplane, Observation, Light Oct 17 1957

25 Autogiro Mail Service, Philadelphia, PA Oct 2 1940 26 Serial No. 3445 Air Corps TR on Performance Estimates

of Autogiro Equivalents of the XO-27A Observation Airplane

Apr 29 1931

27 No. 98-800 Autogiro, Observation Type Specification for Jul 10 1935 28 Report No. 150.1 Resonance in Rotating Wing Aircraft and

Associated Article Aug 19 1942

29 Report No. 541 Service Test Requirements for Kellett YG­1 Autogiro

May 6 1936

30 Kellett YG-1 Autogiro – Additional Documents Various 31 Report ER-060.2 Comparative Performance of Airplane,

Aurigiro and Theoretical Helicopter Kellett Mar 1940

32 Possibilities of the Jump-Off Autogiro by R.H. Prewitt Kellett

Jan 25 1938

33 NACA AR257 Photographic Observations of Blade Motion of the YG-1B Autogiro Equipped with Tapered

May 9 1940

110

 

Rotor Blades 34 PA-36 Blueprints 1938 35 Report ER-192 Study of Effects of using3 Tilt in Hub of

PA-36 Autogiro Autogiro Co. of America Nov 1 1937

36 Report ER-194 Best Combination of Angles on Centralized Hubs Autogiro Co. of America

Nov 10 1937

37 Report ER-195 Study of Effect of Fairing Autogiro Rotor Hubs and Tapering Blades in Plan-Form Autogiro Co. of America

Nov 11 1937

38 Report ER-202 Study of Probable Performance of Modified PA-33 Autogiro Autogiro Co. of America

Jun 28 1938

39 AF Flight Dynamics Lab Reply to Chief, Patents Division, HQUSAF (AF/JACP) and Associated Documentation

Nov 21 1972

40 Copies of Patents Related to Autigiros Various

CONVERTIPLANES 50 1 Report 67-050161 AFFDL-TR-195 The X-19 V/STOL

Technology – A Critical Review May 1967

2 Miscellaneous Tilt-Rotor Papers 1967 3 Report No. 200-947-003 Model Specification for Two

Place, Single-Engine Convertiplane Bell Sep 3 1952

4 Army Air Mobility Study – Advanced Concepts Supplement

Jun 1962

5 Report 200-099-932 Proposal for a Modernized Version of the XV-3 Convertiplane Bell

Sep 26 1960

6 SAE Report 650193 Helicopters and Propeller-Type VTOL Aircraft in the Light of Technologies by W.Z. Stepniewski & M.I. Young Boeing-Vertol

Apr 12-16 1965

7 FW 860 Seitenleitwerk Photos and Technical Data Sep 1979 8 VC-400 Symposium Info (in German) Nov 1967 9 AHS 50th Annual Forum – Aerodynamic Evaluation of the

V-22 Osprey Wing Section by J.C. Narramore & M.K. Farrell Bell & W.K. Grauer Boeing

May 11-13 1994

10 Report No. CER 897 ER on The Results of the Wind Tunnel Testing for the 1/10 Scale Aerodyne Model Contract# Nonr 2566(00)

Jan 30 1959

11 The Domain of the Convertible Rotor by R. Hafner Westland Aircraft Ltd.

Undated

12 AHS 28th Annual Forum #615 Parametric Studies of Instabilities Associated with Large, Flexible Rotor Propellers by Dr. Robert A. Johnson Sikorsky

May 1972

13 AHS 24th Annual Forum Tilt-Proprotor Composite Aircraft, Design State of the Art by K.G. Wernicke Bell

May 1968

14 Planicopter Project II, IIIA, IIIB Undated 15 VC-400 VTOL-Kipp-Rotor (in German) Aug 14 1964

111

16 Report No. 200-094-270 Results of the Wind Tunnel Tests of the Quarter-Scale Semi-Span Model of the XV-3 Tilting-Rotor Convertiplane Contract# AF 33(600)20777

Aug 18 1958

17 NACA TN 3917 Effects of Propeller Location and Flap Deflection on the Aerodynamic Characteristics of a Wing-Propeller Combination for Angles of Attack from 0o to 80o

Jan 1957

18 NASA TN D-318 A Wind Tunnel Investigation of Three Propellers Through an Angle of Attack Range from 0o to 85o

May 1960

19 NASA TN D-730 Aerodynamic Characteristics of Propeller-Driven VTOL Aircraft

Mar 1961

20 Report No. 200-099-201 Calculated Weight and Balance XV-3 Convertiplane Contract# AF 33(600) 20777

Nov 1 1954

21 VTOL Articles Various 22 NASA CR 177452 Civil Tiltrotor Missions and

Applications: A Research Study Contract# NAS2-12393 Jul 1987

23 JVX “What an Opportunity” Presentation Slide Printouts Apr 20 1982 24 Technology Assessment of Capability for Advanced Joint

Vertical Aircraft (JVX) Industry Debriefing Jun 28 1982

25 XV-15 Articles and Photos Various 26 XV-3 Articles and Photos Various 27 Model 732 Variants Conceptual Diagrams Undated 28 V-22 Photos, Articles Various 29 V22/MV22 5 Theses 1988-1989 30 AHS 40th Annual Forum JVX Design Update by Stanley

Martin, Jr. & William B. Peck Boeing-Vertol May 16-18 1984

31 NASA TM 84293 Dynamic Structural Aeroelastic Stability Testing of the XV-15 Tilt Rotor research Aircraft

Dec 1982

32 Report AD-B102 592 Evaluation of XV-15 Tilt Rotor Aircraft Concept for JVX Missions

May 12 1986

33 Report AD-A134 642 Airloads on Bluff Bodies, with Application to the Rotor-Induced Downloads on Tilt-Rotor Aircraft

Sep 1983

34 AIAA-83-2695 Frequency-Domain Identification of XV­15 Tilt-Rotor Aircraft dynamics

Nov 16-18 1983

35 Report AD920906 Low-Disc-Loading Helicopter and Tilt-Rotor Aircraft Study Bell

Apr 1974

36 An Analysis of Low-Disc-Loading VTOL Aircraft Types by Robert L. Lichten Bell

Jan 10-13 1966

37 Expanding Tilt Rotor Capabilities by J.M. Drees Bell 1988 38 Advanced Helicopter Technology Seminar Jul 18 1967 39 Prop-Rotor Info Various 40 AFFDL-TR-70-44 Configuration Design Analysis of a

Prop/Rotor Aircraft Apr 1970

41 General Considerations for Response of Tilting Rotors to Sharp Edge Gusts by R.F. Klingloff Sikorsky

Nov 4 1969

112

42 VTOL Transportation Briefing May 18 1966 43 NASA TM 81280 Historical Overview of V/STOL

Aircraft Technology by Seth B. Anderson Mar 1981

44 Report D266-099-104 Composite Research Aircraft Design Study – Weight and Balance Contract# DA-44­177-AMC-373(T)

May 1966

AUTOGIROS 51 1 Report No. 146X90-2 A Proposal to Appraise the Modern

Usefulness of Autogiros Kellett Aircraft Dec 12 1958

2 Rotary Wing Kite (partial) Lt. R.N. Gottfried (from German)

Undated

3 Report No. UDSE-TR-74-03 Autogiro Feasibility Study Design and Cost Analysis by F. Gerard Albers Univ. of Dayton

Aug 1974

4 McCulloch Autogiro Pamphlets 1966-1968 5 The Police Autogiro – Plan For Development Sep 1972 6 McCullogh Autogiro Papers 1968 7 Report No. WSDS 69-61 Hanson Autogiro Study Dec 1969 8 FA-330 German Submarine (U-Boat) Kite Oct 12 1948 9 Report No. 158X90-1 The 1960 Autogiro A New

Observation and Liaison Aircraft Kellett Feb 1959

10 Kinedyne 2 Autogiro Cessna C.A. 1958 11 Report No. 3 Super-STOL A Proposal For general

Aviation by Thomas F. Hanson May 1969

12 Autogiro – Miscellaneous Papers Undated 13 Report No. USDE-TR-75-09 Simulation of Autogiro

Performance by F. Gerard Albers & David L. Moorman Univ. of Dayton

Oct 1975

14 NACA Confidential Memorandum Report Control-Force and General Performance Tests of Kellett YG-1 Autogiro

Mar 27 1936

15 The Hafner Gyroplane by Raoul Hafner Feb 1938 16 Kellett YG-1 Wind-Tunnel and Flight Tests C.A. 1937 17 Reports and Memoranda No. 1859 General Investigation

into the Characteristics of the C.30 Autogiro Mar 1939

18 Report No. Z-812 Apparent Aerodynamic Limitations of Rotary Wing Aircraft in Towed Flight Eastern Rotorcraft

Jul 15 1948

19 Reports and Memoranda No. 1154 Wind Tunnel Experiments on a Model Autogiro at Small Angles of Incidence

Mar 1928

20 Reports and Memoranda No. 1116 Wind Tunnel and Dropping Tests of Autogiro Models

Nov 1926

21 Report No. 160.37Flight Performance Tests of the XR-3 Autogiro Kellett Aircraft

May 26 1944

22 Report No. ASTDN FTR 70-6 Rotorglider Discretionary Descent Concept by Robert W. Markland

Feb 1970

113

23 Aircraft Carrier by Jerry O’Rourke Feb 19 1975 24 Report No. LR 24151 STOL/Autogiro Vehicle Study for

Mass Urban Transportation Lockheed-California Dec 1970

25 Report No. R-70-0-3061-A Proposal for the Kaman Model K-15 Utility and Liaison Gyroplane Kaman

Apr 6 1955

26 NACA Memorandum Report Full-Scale Wind-Tunnel and Flight Tests of a YG-1 Autogiro

Aug 26 1937

27 Report No. G-101 Analysis of Giro-Glider AGA Aviation Corp.

Jan 20 1943

28 The Autogiro – Tomorrow’s Aircraft Today by Robert K. Clark

1975

29 Cyclogiro Information C.A. 1967 30 The Roadable Autogiro by B. Lindenbaum Nov 1971 31 Drone Autogiro –AISA GU-100 Jun 14 1973 32 FA223 Equipment Test Photos Undated 33 Comparative Evaluation of the Kinedyne Cessna Undated 34 Report No. 12-170.1 Design Study for KD-2X Giro

Incorporating Direct Take-Off and Direct Landing Kellett Sep 24 1937

35 The Autogiro – A Business Opportunity Undated 36 Testimony Before the Committee on Military Affairs of the

House of Representatives Apr 26 1938

37 Report No. R-80 Aerodynamic Performance Characteristics – Kaman Model K-15

Apr 6 1955

38 Autogiro Transparencies C.A. 1965 39 Autogiro Proposal to Aerospace Corp. by Nichols Jan 1973 40 Extra Figures and Tables for Police Autogiro Report C.A. 1972 41 Schluter ROBBE Autogiro 1990 42 Autogiro – Miscellaneous Post WWII Various 43 Engine Off Landings Nov 13 1947 44 NACA TN No. 741 Observations in Flight of the Region

of Stalled Flow Over the Blades of an Autogiro Rotor Dec 1939

45 NACA TN No. 1267 Flight Tests of a Helicopter in Autorotation, Including a Comparison with Theory

Apr 1947

46 R. & M. No. 1727 The Effect of Blade Twist on the Characteristics of the C.30 Autogiro

1936

47 R. & M. No. 1802 A Rough Estimate of the Twist of Autogiro Blades in Flight

1937

48 Technique of Handling the Direct-Control Autogiro by Lou Levy Kellett

Undated

AUTOGIROS & AUTOGIRO GLIDERS/KITES 52 1 Report No. 01954-2-T Autorotating Wings: An

Experimental Investigation Contract# DAHCO-4-68C­0027 Univ. of Michigan

Jun 1970

2 AISA Autogiro Sketch and Specifications Undated 3 NACA TN 209 Tests of Rotating Cylinders Dec 1924

114

5

10

15

20

25

4 NACA TM 367 Application of the “Magnus Effect” to the Wind Propulsion of Ships

Nov 17 1924

Report No. R&M, No. 1009 Experiments on the Flow Behind a Rotating Cylinder in a Water Channel

May 1925

6 Report No. R&M, No. 1018 Experiments on the Air Forces on Rotating Cylinders

Jun 1926

7 Report No. R&M, No.1410 Experiments on the Flow Past a Rotating Cylinder

Mar 1931

8 Report No. R&M, No. 1623 On the Effect of Discs on the Air Forces on a Rotating Cylinder

Jan 5 1934

9 Aerodynamics of Flight Mechanics of Magnus-Rotor Bomblets Volume I. Literature Search by James E. Brunk Contract# F08635-67-C-0135

1968

Report No. 1430.7 Wind Tunnel Test No. 1009 Test of Kellet XR-Fuselage

May 1944

11 Performance Substantiation for Kinedyne Proposal Cessna Feb 5 1958 12 Proposal – Model CH-3 Kinedyne Design – Engineer – 2

Prototypes Flight Test Cessna Apr 21 1958

13 The Kinedyne Concept Cessna Aircraft Co. C.A. 1958 14 Report No. 146X90-1 A Proposal to Appraise the Modern

Usefulness of Autogiros Kellett Sep 29 1958

Report No. 146X90-2 A Proposal to Appraise the Modern Usefulness of Autogiros Kellett

Dec 12 1958

16 Handbook of Service Instructions for the Model YO-60 Liaison Observation Autogiro Kellett

Undated

17 Report No. 56-115 Proposal for the Construction and Test of a Power Compounded Vertical Take-Off Autogiro Hiller

Dec 1956

18 Report No. 158X90-1 The 1960 Autogiro – A New Observation and Liaison Aircraft Kellett

Feb 1959

19 Report No. 420-1-23 XR-1 Aircraft Contract# W535 ac­15375 Platt-LePage

C.A. 1945

Autogiro Description Material Letter Garrett Airesearch Dec 3 1973 21 Engineering Theory of the Autogiro by Juan de la Cierva

(with handwritten corrections) (probably late 1920’s) Undated

22 Report No. ER-111 Proposed Additions to “The Theory of the Autogiro” Autogiro Co. of America, Inc.

Apr 1933

23 NACA Report No. 523 The Influence of Wing Setting on the Wing Load and Rotor Speed of a PCA-2 Aurogiro as Determined in Flight

1935

24 NACA TN 581 A Study of Autogiro Rotor-Blade Oscillations in the Plane of the Rotor Disk

Sep 1936

NACA TM No. 879 Static Longitudinal Stability and Longitudinal Control of Autogiro Rotors

Oct 1938

26 TR No. 330-45 Focke-Achgelis Autogiro Type Fa 330 Sep 1945 27 Item No. 12 File No. XXVIII-21 CIOS German Submarine C.A. 1945

115

Rotary Wink Kite 28 Report No. 33200 “Rotochute” Rotary Wing Glider-Kite

General Electric Co. Oct 25 1946

29 Report No. DCR-292 Concept Description of Autogiro Air-Train System (AATS) Dynasciences Corp.

Nov 1968

30 Report No. AU-112 Model Specification – Rotary Wing Glider G&A Aircraft, Inc.

Sep 1 1944

31 Autogiro Drone Papers, Charts and Photos Northrop/Radioplane

Various

32 Autogiro Project – ARPA’s Visit to Spain May 2-4 1973 33 Alternate RPV Configuration Garrett Dec 3 1973 34 An Autogiro RPV Presentation Garrett Undated 35 Report No. R&M No. 1116 Wind Tunnel and Dropping

Tests of Autogiro Models Nov 1926

36 Report No. R&M No. 1131 Lift and Torque on an Autogiro on the Ground

Jul 1927

37 Report No. R&M No. 1802 A Rough Estimate of the Twist of Autogiro Blades in Flight

1937

38 NACA TN 741 Observations in Flight of the Region of Stalled Flow Over the Blades of an Autogiro Rotor

Dec 1939

39 Report No. R&M No. 1859 General Investigation into the Characteristics of the C.30 Autogiro

Mar 1939

40 Report No. R&M No. 1727 The Effect of Blade Twist on the Characteristics of the C.30 Autogiro

1933

41 Farrington Aircraft Co. Autogiro Information 1993 42 Extension of Compound Helicopter Performance by Means

of the Telescoping Rotor by Evan A. Fradenburgh Sikorsky

1969

43 Special Report on VFW Compound Aircraft Jan 17 1968 44 Tests of the German Submarine Rotary Wing Kite, Fa-330 1948 45 A Study of Design and Economics of Rotary Wing Gliders

by Igor B. Bensen Kaman Apr 26 1951

46 NACA Report No. 434 Lift and Drag Characteristics and Gliding Performance of an Autogiro as Determined in Flight

1932

47 NACA Report No.523 The Influence of Wing Setting on the Wing Load and Rotor Speed of a PCA-2 Autogiro as Determined in Flight

1935

48 NACA Report No.536 Wind-Tunnel Tests of a 10-Foot-Diameter Gyroplane Rotor

1935

49 NACA Report No.552 Wind-Tunnel Tests of a 10-Foot-Diameter Gyroplane Rotor

1936

50 NACA Report No. 600 An Analysis of the Factors That Determine the Periodic Twist of an Autogiro Rotor Blade, with a Comparison of Predicted and Measured Results

1937

51 NACA Report No. 623 A Study of the Torque Equilibrium 1938

116

on an Autogiro Rotor 52 Testimony before the Military Affairs Committee of the

House of Representatives by Harold F. Pitcairn Autogiro Co. of America

Apr 26 1938

53 McCullouch Aircraft Corp Status Summary Jul 1 1971 54 The Autogiro – A Business Opportunity by Bell Sep 15 1975 55 Tomorrow’s Aircraft Today by R.K. Clark 1976 56 McCulloch Aircraft Articles, Pamphlets and Brochures Various 57 United Technical Industries Business Plan Volume 1-Intro

and Executive Summary Jul 1983

58 United Technical Industries Business Plan Volume 2 & 3 – Detailed Business Plan Appendices

Jul 1983

59 Autogiro Miscellaneous Articles and Photos Various

COMPOUND HELICOPTERS, CONVERTIPLANES, TIP-MOUNTED POWER

53 1 Proposal for Engineering Study of Medium Transport Convertible Aircraft No. 3A

Nov 11 1957

2 Report No. R-527A UH-2 Helicopter High-Speed Flight Research Program Utilizing Jet Thrust Augmentation Final Report (Draft) Contract# DA 44-177-AMC-105(T) Kaman

Nov 1964

3 Report No. PR-564 Preliminary Design Study of VTOL Rotary Wing Composite Aircraft – Technical Proposal Contract# RFP AMC-177-65 Neg. 91 Boeing-Vertol

Jul 16 1965

4 Report No. 58-139 A Design Study of Helicopters Powered by Rotor Tip Mounted Turbojet Engines Contract# Nonr 1814(00) Hiller

Oct 1958

5 VTOL Boundaries by R.B. Lightfoot Sikorsky Feb 14 1962 6 A VTOL Progress Report for the Four-Ton Payload

Sikorsky Jan 17 1964

7 Notes on Studies of VTOL and V/STOL Aircraft by R.G. Stutz Sikorsky

Jun 1963

8 Report No. ES 40495 A RVX Study – A Comparison of Mother/Daughter and Single Aircraft Concepts Douglas

Sep 9 1961

9 Report No. UP-42 Study of Proprietary Ideas Concerning the Aerodynamics of Retractable Rigid Rotors with Circulation Control by Blowing Air Vehicle

Jun 1968

10 NASA Literature Search No. 5331 Stoppable Rotor Aircraft

Dec 1 1967

11 Convertiplane Interest Grows Fast by Robert McLarren AW&ST

Dec 26 1949

12 Model D2064 Propulsion System Blueprint Lockheed-Georgia

Mar 14 1961

13 AGARD Conference ( 2 papers on Fluid Controlled Stoppable Rotors)

Sep 20-23 1971

14 Report No. D181-945-008 Bell Aerosystem X-22 Proposal May 1956

117

with Photos 15 Aerodyne Brochure Dornier System (in German) Undated 16 Shrouded/Ducted Prop Illustrations Various 17 Report No. 84-X-5 Vectored Thrust Take-Off and Landing

Recoverable Strike RPV: Design Study Piasecki Nov 22 1973

18 Ducted Prop and Ring Wing Various 19 Report No. 7064 VTOL Unloaded Rotor Compound

Helicopter Contract# DA 44-177-TC-588 McDonnell Feb 1 1960

20 “MODUS” High Speed VTOL Reconnaissance Aircraft VMAX

Jan 1995

21 Report No. 8125 Model 177 VTOL Technical Proposal Tri-Service Transport McDonnell

Apr 3 1961

22 Report No. 7223-953001 V/STOL Capability Bell March 1965 23 McCullouch J-2 Gyroplane Brochure Undated 24 The J-2 and How to Fly it. McCullouch 1970 25 Convair VTOL/STOL Handbook Undated 26 Report NO. NB 63-228 The Northrup All Mechanical

Flight Control System for VTOL Aircraft and Reentry Vehicles

Sep 1963

27 Report No. 1272 A Project Suggestion for a VTOL RPV Centro Corp.

Undated

28 Current Sikorsky Models Brochure Jun 1966 29 Statement by R. Hafner and Extracts from Patent

Applications Sep 1938

30 Kinedyne Concept Brochure Cessna Undated 31 Sikorsky S-65-300 Compound V/STOL Transport Volume

I Technical Undated

32 Report No. LR 21049 Advanced VTOL Naval Aircraft Study Final Report Contract# N00019-67-C-0261 Lockheed-California

Jun 10 1968

33 Report No. 4197 The V-1B Convertiplane McDonnell C.A. 1955

34 Report No. 7376 (Supplement to No. 7064) Substantiating Data on the Unloaded Rotor V/STOL Transport Aircraft McDonnell

Feb 1 1960

35 Miscellaneous Papers Undated

COMPOUND & RIGID ROTOR HELICOPTERS 54 1 Report No. 285-17 (62-17) Hot Cycle Design and

Development Program Technical Summary Report Contract# AF 33(600)-30271 HTC

Mar 1962

2 Report No. HTC-AD-65-15 Rotor/Wing Concept Study, Summary TR – Volume II – Appendices A, B, C, D, E, and F Contract# Nonr-4588(00) HTC

Sep 1965

3 Report No. HTC-AD-65-37 Rotor/Wing Concept Study, Supplementary Study Report Contract# Nonr-4588(00)

Feb 1966

118

HTC 4 Report No. HTC-AD-67-3 Rotor/Wing Series VI Wind

Tunnel Test 7-Foot Diameter Model in the NASA LRC 30­by-60-Foot Wind Contract# Nonr-4588(00) HTC

Apr 1968

5 Report No. HTC-AD-69-12A Rotor/Wing Final TR Contract# Nonr-4588(00) HTC

Mar 1970

6 Stowed Rotor Assault Transport Parametric Study Boeing-Vertol

1965

7 NASA TN D-5232 Wind-Tunnel Investigation of Steady-State Aerodynamics of a Composite-Lift VTOL Aircraft Model

Jun 1969

8 NASA TN D-5256 A Wind-Tunnel and Analytical Study of the Conversion from Wing Lift to Rotor Lift on a Composite-Lift VTOL Aircraft

Jun 1969

9 NASA TN D-5945 Wind-Tunnel Investigation of Various Small-Scale Rotor/Wing Configurations for VTOL Composite Aircraft in the Cruise Mode

Oct 1970

10 WADC TR 55-410 WADC Rapid Performance Prediction Method for Compound Type Rotorcraft

Mar 1959

11 USAAVLABS TR 68-31 Hot Cycle Rotor/Wing Composite Research Aircraft Contract# DA 44-177-AMC­338(T)

Aug 1968

12 USAAVLABS TR 68-32 Tilt Prop-Rotor Composite Research Aircraft Contract# DA 44-177-AMC-373(T)

Nov 1968

13 NASA CR 112152 Rotor System Research Aircraft Predesign Study Final Report Volume I Summary and Conclusions Contract# NAS1-11228

Oct 6 1972

14 NASA CR 112153 Rotor System Research Aircraft Predesign Study Final Report Volume II Conceptual Study Report Contract# NAS1-11228

Oct 6 1972

15 NASA CR 112154 Rotor System Research Aircraft Predesign Study Final Report Volume III Predesign Report Contract# NAS1-11228

Oct 6 1972

16 NASA CR 112155 Rotor System Research Aircraft Predesign Study Final Report Volume IV Preliminary Draft Detail Specification Contract# NAS1-11228

Oct 6 1972

17 Report No. FT23-4R-64 Military Research Evaluation of the Lockheed XH-51A Rigid Rotor Helicopter

Jan 7 1964

18 The Conversion of the Rotor/Wing Aircraft by R.J. Huston & J.P. Shivers NASA

Sep 11-13 1967

19 Composite Aircraft Design by LeRoy H. Ludi USAAVLABS

May 10-12 1967

20 Rotor Systems Research Aircraft Predesign Summary Review

Sep 22 1972

119

21 Report No. LR 26175 VTOL Strike RPV Study Contract# F 33657-74-C-0190 Lockheed-California

Dec 12 1973

22 Possibilities of Compound Helicopters – Status 1968 by Dr. Richard M. Carlson Lockheed-California

Mar 7 1968

23 Report No. D8-0554 Evaluation Report of the Rotafix Concept Boeing-Vertol

Jan 1968

24 BRL MR 1850 Composite V/STOL Utility/Logistics Aircraft, Speed Versus Payload and Productivity

Jun 1967

25 Report No. 2346 Preliminary Stability and Control Report Model 82 Contract# AF 33(038)-28075 McDonnell

Nov 12 1951

26 Report No. SER-2554 An Examination of the Stability and Control Problems of a Compound Helicopter Contract# AF33(616)2628 Sikorsky

May 12 1955

27 Report No. SER-2557 Proposed Work Statement Extended Investigation of Long Range Helicopter Contract# AF33(616)-2628

Jun 15 1955

28 Report No. SER-2569 Proposed Work Statement – Study Toward Compound Helicopter Performance Sikorsky

Jan 23 1956

29 Report No. LR 19533 Composite Research Aircraft – Preliminary Design Study and Proposal for Full-Scale Follow-On Program Volume I – Technical Contract# DA 44-177-AMC-372(T) Lockheed-California

May 1966

30 Report No. LR 19539 Composite Research Aircraft- Summary Report Lockheed-California

May 1966

31 Report No. LR 19755 Advanced Transport Aircraft – 1975-1985 Lockheed-California

May 19 1966

32 Report No. LR 21283 A Summary of Stopped Rotor Research and Development at the Lockheed-California Company

Jan 22 1968

33 XV-1 Photos and Clippings 1966 34 Miscellaneous Loose Pages Concerning V/STOL

Transport 1960-1961

35 Roles and Missions Documents 1956 36 Compound Helicopter Photos and Notes Various 37 Convertiplane Development Project Folder Contract AF

33(600) 22222 1952-1956

SERIES VII: SR-175, Tri-Service Transport and V/STOL Transports, 1938-1990

Box File Description Date

SR-175 + SYMPOSIUMS 55 1 AHS, Inc.: Proceedings of the Sixteenth Annual National

Forum May 11-14 1960

2 USAF AFSC: Report: Beyond the Horizon: Flight in the Atmosphere, 1975-1985 Volume III Annexes Vertical

Jan 1967

120

Takeoff and Landing 3 SR-175 V/STOL Logistic Aircraft Study Vol. I Appendix;

Contractor Report Summaries Jun 1960

4 Proceeding of Rotating Wing Aircraft Meeting at Franklin Institute

Oct 1938

5 Conference on V/STOL and STOL Aircraft Ames Research Center

Apr 4-5 1966

6 Report 7277 V/STOL Logistics Aircraft Study 1965-1970 Time Period McDonnell Aircraft Corp

Feb 12 1960

7 Second Convertible Aircraft Congress Proceedings Dec 12 1952 8 USAF AFSC Report: Beyond the Horizon: Flight in the

Atmosphere, 1975-1985 Volume III Vertical takeoff and Landing

Jan 1967

9 Avenues for Research 1966 US Army Aviation Material Laboratories

Jun 1966

10 Presentation to the Ad Hoc Group on Evaluation of V/STOL Aircraft, Princeton, NJ Lockheed

Nov 11 1959

11 Proceedings of 1st National V/STOL Aircraft Symposium Supplement

Nov 3-4 1965

12 USAF AFSC Report: Beyond the Horizon: Flight in the Atmosphere, 1975-1985 Volume III Vertical Takeoff and Landing

Jan 1967

13 Proceedings of 1st National V/STOL Aircraft Symposium Nov 3-4 1965 14 AIAA/NASA Ames V/STOL Conference: A Collection of

Technical Papers Jun 6-8, 1977

15 Proceeding of Rotating Wing Aircraft Meeting at Franklin Institute

Oct 1938

16 Proceeding, Third Cal/AVLabs Symposium: Aerodynamics of Rotary Wing and V/STOL Aircraft Volume I Rotor/Propeller Aerodynamics-Rotor Noise

Jun 18-20 1969

17 Proceeding, Third Cal/AVLabs Symposium: Aerodynamics of Rotary Wing and V/STOL Aircraft Volume II Wind Tunnel Testing-New Concepts in Rotor Control

Jun 18-20 1969

18 AHS, Inc.: Proceedings of the Fourteenth Annual National Forum

Apr 16-19 1958

19 3-Ring Binder – Data and Diagrams of Various Helicopter Projects Including Kellett Project 19, G. & A. Model 49, Bell Model D-41 and Sikorsky Model R-5D

Undated

20 USAF AFSC Report: Beyond the Horizon: Flight in the Atmosphere, 1975-1985 Volume III Vertical Takeoff and Landing

Jan 1967

TRI-SERVICE TRANSPORT

121

5

10

15

20

25

56 1 NA01H-101 Tri-Service VTOL Transport Aircraft – Proposal Summary North American Aviation, Inc.

Apr 3 1961

2 Tri-Service VTOL Transport Sketches and Blueprints North American Aviation, Inc.

1961

3 Report PDR-511A-11 Helicat Aerodynamic Model and Full Cyclic Prop/Rotor System Vol. 1 Technical Proposal Grumman

Oct 1970

4 Report PDR-511A-12 Helicat Aerodynamic Model and Full Cyclic Prop/Rotor System Vol. 1 Price Proposal Grumman

Oct 1970

Grumman Helicat Presentation c.a. 1970 6 NASA Memo 8-4-59A Full-Scale Wind-Tunnel

Investigation of the Longitudinal Characteristics of a Tilting-Rotor Convertiplane

c.a. 1959

7 Prop-Rotor Stability at High Advance Ratios – Article Undated 8 Design and Developmental Considerations of the X-19

VTOL Aircraft Curtiss-Wright Undated

9 Sikorsky Concept Photos VTOL Transport Undated Advanced VTOL Concepts Presentation Boeing Oct 1967

11 XV-15 Presentation Vugraphs Undated 12 Bell Helicopter Letter, Pamphlets XV-3/XV-15 Feb 23 1978 13 Report 299-099-128 Technical Considerations for Low-

Disc-Loading V/STOL Aircraft of the Fixed-Wing and Tilt-Wing Configurations

Dec 23 1959

14 JVX What an Opportunity Presentation Apr 20 1982 Tilt-Rotor Articles and Pamphlets Various

16 D246-099-020 V/STOL Transport Aircraft Study 1965­1970 Bell

Mar 1 1960

17 Bell Helicopter Cost and Engineering Proposals, Tri-Service VTOL Transport Aircraft

Mar-Apr 1961

18 D252-099-001 Summary Report D252 Tri-Service Transport Aircraft Bell

Mar 31 1961

19 D252-099-003 Stability and Control Analysis D252 Tri-Service Transport Aircraft Bell

Mar 30 1961

D252-099-004 Estimated Weight and Balance D252 Tri-Service Transport Aircraft Bell

Mar 30 1961

21 D252-099-005 Structural Description and Design Data D252 Tri-Service Transport Aircraft - Bell

Mar 30 1961

22 D252-099-006 Structural, Ground and Flight test Program D252 Tri-Service Transport Aircraft - Bell

Mar 30 1961

23 D252-099-007 Power Plant and Drive System Installation D252 Tri-Service Transport Aircraft - Bell

Mar 30 1961

24 D252-099-008 Maintenance and Support Data D252 Tri-Service Transport Aircraft - Bell

Mar 30 1961

D252-099-009 Dynamics Analysis D252 Tri-Service Transport Aircraft - Bell

Mar 30 1961

122

26 D252-947-001 Detail Specification D252 Tri-Service Transport Aircraft - Bell

Mar 30 1961

27 Report 300-099-003 Advancement of PropRotor Technology Task I-Design Study Summary Contract# NAS 2-5386 Bell

Sep 3 1969

28 Boeing Document D-215-10000-1 Determination of design Criteria and Demonstration of Technology of s Prop/Rotor Aircraft R&D Interim Report R&D-3-FDL

Aug 1969

29 Boeing Document D-215-10000-1 Detail Design of Critical Components for a Prop/Rotor Aircraft Phase II of Determination of Design Criteria and Demonstration of Technology of s Prop/Rotor Aircraft

Jul 1970

30 Helicat Aerodynamic Model and Full Cyclic Prop/Rotor System Volume 1 – Technical Proposal (Revision)

Undated

31 Sikorsky S-65-200 Compound Helicopter Brochure Undated 32 Report No. LR 21793 Proposal for Study of Propulsion

System Requirements for Advanced Rotary Wing Compound and Composite Aircraft Lockheed-California

Sep 1968

33 Report No. FT-66-1 Analysis of VSTOL Aircraft Configurations for Short Haul Air Transportation Systems Contract# C-85-65 (Dept. of Commerce)

Nov 1966

34 Report No. 535 Dynamic Stability Analysis of a VTOL Vectored Slipstream Vehicle During Transition Contract# Nonr 1858(01) and (14) Princeton Univ.

Apr 1961

TILT-WING/PROPELLOPLANE 57 1 Report 58-136 Remote Controlled Free Flight Test of a 1/8

Scale Model X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller

Oct 31 1958

2 Grumman Tilt-Wing Design 242 – Miscellaneous Papers and Pictures

Undated

3 Boeing-Vertol Model 119F Proposal PR 394 Undated 4 Report 56-60 Tilt-Wing Propelloplanes for Transport-

Rescue Missions Hiller Jun 1956

5 ARD-207 VTOL Amphibious Assault Transport Systems 1962-1967 Hiller

Jan 30 1959

6 Product Analysis of Tilt Wing Propelloplane Type VTOL Aircraft by J. B. Nichols Hiller

Undated

7 VTOL/VSTOL Logistic Transport Tilt Wing Propelloplanes Contract AF SR 175 Hiller

Feb 1960

8 Report 461.3 A Simplified Theoretical Investigation of a Wing-Propeller Combination Through a Range of Angle­Of-Attack from 0 to 90 Degrees and a Comparison with Experimental Results

Oct 15 1955

9 Report 461.31 A Simplified Theoretical Investigation of a Wing-Propeller Combination Through a Range of Angle-

Apr 6 1956

123

Of-Attack from 0 to 90 degrees II – Partial Wake Deflection

10 Propelloplane Transport Study Summary Report Contract# Nonr-1657(00) Hiller

May 15 1956

11 Tilt Wing Propelloplane Design Requirements by Joseph Stuart III Hiller Helicopters Plus Slides and Photos

Oct 7-9 1956

12 NASA Memorandum 11-3-58L Force-Test Investigation of the Stability and Control Characteristics of a 1/4 –Scale Model of a Tilt-Wing Vertical-Take-Off-and-Landing Aircraft

Nov 20 1958

13 NASA Memorandum 11-4-58L Flight Investigation of the Stability and Control Characteristics of a 1/4 –Scale Model of a Tilt-Wing Vertical-Take-Off-and-Landing Aircraft

Nov 20 1958

14 Report CS-1790 SER-50145 U.S.NAVY Tri-Service VTOL Prototype Transport Engineering Proposal Part I Sikorsky

Apr 3,1961

15 Report CS-1790 SER-50145 U.S.NAVY Tri-Service VTOL Prototype Transport Engineering Proposal Part II Sikorsky

Apr 3 1961

16 Report 59-34 Airplane Stability and Control X-18 Tilt-Wing Test Bed Contract# AF 33(600)32749 Hiller

May 15 1959

17 Report 57-9 Aerodynamic Data for Structural Analysis X­18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)32749 System No. 607A Hiller

Feb 21 1958

18 HSER 2407 Blade for Sikorsky Tri-Service VTOL Sikorsky

Mar 28 1961

19 SER 50146 Tri-Service VTOL Prototype Transport Proposed Ground Test Program Sikorsky

Apr 3 1961

20 SER 50147 Tri-Service VTOL Prototype Transport Proposed Flight Test Program Sikorsky

Apr 3 1961

21 SER 50148 Tri-Service VTOL Prototype Transport Proposed Detail Specification Sikorsky

Mar 29 1961

22 SER 50149 Tri-Service VTOL Prototype Transport Supporting Research Report for Engineering Proposal Sikorsky

Apr 3 1961

23 Report 57-58-1 Estimated Flight test Performance X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 System No. 607A Hiller

May 31 1957

24 Report 57-58-2 Estimated Flight Test Performance X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 System No. 607A Hiller

May 31 1957

25 Breguet 941 VTOL Transport Detail Specification Summary Report for Tri-Service Prototype Aircraft by Harlan D. Fowler

Apr 9 1961

26 U.S.NAVY Tri-Service VTOL Prototype Transport Cost Proposal Refer to CS 1790 Sikorsky

Apr 14 1961

124

27 Report 58-74 An Analysis of the Variation of Pitching Moment in Transition Flight X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 System No. 607A Hiller

May 27 1958

28 Report 56-94 Stability and Control Analysis Aircraft, Tilt-Wing, VTOL Test Bed X-18 Contract# AF 33(600)-32749 System No.451L Hiller

Oct 5 1956

29 SR 175 VTOL/VSTOL Logistic Transport Tilt Wing Propelloplanes

Feb 12 1960

V/STOL TRANSPORT/LIFT FANS & FAN IN WING 58 1 Report G-18-35 VTOL/STOL Logistics Aircraft

Parametric Study – 1965-1970 Time Period Ryan Jan 23 1960

2 Report A 35-52-2 Preliminary Design Report Study of Submerged Fan Type VTOL Aircraft Contract# AF33(616)-6605 Ryan

Feb 15 1960

3 Lift Fan Miscellaneous – 1) Concept Photos (6); 2) VZ-11 Pamphlet; 3) Vertiflite Article Feb 1964 – Lift Fan Concept

1964

4 FTC-TR-66-30 Flight Evaluation of the XV-5A VSTOL Aircraft

Mar 1967

5 XV-5A Lift Fan VSTOL A/C Flight Test Accomplishments GE Flight Propulsion Div.

1967

6 Report 63B032A Operational V/STOL Aircraft Evaluation Program – Volume III – Aircraft Characteristics Ryan

Aug 13 1963

7 IAS Paper No. 63-27 Characteristics of Aircraft with Lifting-Fan Propulsion Systems for V/STOL by Robert H. Goldsmith and David H. Hickey

Jan 21-23 1963

8 AIAA Paper No. 69-200 Deaign Concept for V/STOL Intercity Jet by Peter G. Kappus GE Engines

Feb 17-19 1969

9 Convertible V/STOL Propulsion Systems – Large Engines GE Flight Propulsion Div.

Sep 1961

10 NASA TN D-5695 Wind-Tunnel Investigation of a V/STOL Transport Model with Six Wing-Mounted Lift Fans

Mar 1970

11 NASA TN D-4322 Static and Dynamic Longitudinal Stability Derivatives of a Powered 0.18 Scale Model of a Fan-In-Wing VTOL Aircraft

Feb 1968

12 NAS2-5499 Advanced Lift Fan Aircraft Study McDonnell Aircraft

Jun 2 1970

13 TSP-6415 Lift Fan Technology Undated 14 NA-66-1287 Fan and Inlet Performance from an

Experimental Investigation of a Multi Fan-In-Wing V/STOL Model North American

Jan 4 1966

15 R60FPD149 Volume III – Propulsion System Data Parametric Study SR-175 VTOL/STOL Logistics Aircraft

Mar 1960

125

1965-1970 Period GE Flight Propulsion 16 WADD TR 60-374 Volume I Study of Submerged Fan

Type VTOL Aircraft Ryan May 25 1960

17 Report G-29-42 Parametric Analysis Report Study of Submerged Fan Type VTOL Aircraft Ryan

Sep 8 1959

18 GE Propulsion Magazine Vol. I No. 11, 17(2copies),21,23 Undated 19 Technical Discussion on the Tip Turbine Driven Lift and

Lift/Cruise Fan Propulsion System GE Flight Propulsion Undated

20 Lift Fan data for V/STOL Medium Logistics Transports GE Flight Propulsion

Jan 27 1961

21 Report 22272-1 Strike Escort Rescue Aircraft Ryan Model 222 – Summary Aircraft Specification

Dec 7 1966

22 WADD TR 60-374 Volume II – Study of Submerged Fan Type VTOL Aircraft GE

Mar 1960

23 NASA TN D-4092 Aerodynamic Characteristics of a Large-Scale V/STOL Transport Model with Lift and Lift-Cruise Fans

Aug 1967

24 Report G-52-6 The feasibility of the VERTIFAN Concept Ryan

Feb 18 1958

25 Report A35-52-1 Aircraft Design Studies Report of Submerged Fan Type VTOL Aircraft Contract# AF33(616)-6605 Ryan

Nov 15 1959

26 Report 63B033 (Partial) untitled Ryan Undated 27 Report 64B002 Proposal for V/STOL Operational

Evaluation Aircraft Program Part I – Aircraft Preliminary Specification Ryan

Feb 10 1964

V/STOL SHORT HAUL TRANSPORT 59 1 Parametric Investigation on STOL Aircraft FIAT Jun 20 1960

2 Report 61B118 Proposal for a Flex Wing STOL Assist System for a USAF F-100D Aircraft Ryan

Dec 1 1961

3 Report AER-E1R-12759 V-451 Close Support STOL Chance Vought

C.A. 1961

4 Report DAC-56096 Preliminary Results – Advanced Tactical Transport Studies (with inserts) Douglas

Mar 23 1967

5 Report LB-30899 Proposal for an STOL to V/STOL 10-12 Ton Payload Assault Transport Douglas

Jun 8 1962

6 Soviet YAK Freehold and SU-7 Fighters – Negative Copy from AWST

Apr 14 1969

7 Report 9D-F-11 Research and Development Program for Low Airspeed Control Techniques as Applied to STOL Vehicles (Preliminary Draft) Honeywell

Oct 15 1969

8 Report D3-8514-2 Low-Wing-Loading STOL Transport Ride Smoothing Feasibility Study Boeing

Jan 1971

9 Report D6-8543 Design Considerations for a Ten Ton Tactical Transport Boeing

Jul 1962

126

10 Report D180-14413-1 STOL Tactical Aircraft Investigation – Final Program Review Contract#F33615­71-C-1757 Boeing

Jan 24 1973

11 FTD-HC-23-179-69 Some Problems Concerning Airplanes with Short Start and Landing Distances by Z. Brodski Soviet

May 11 1970

12 “Compound Propulsion System” for Particular Application on Short Take-off and Landing Airplanes and Flying Boats (S.T.O.L.) FIAT

Sep 16 1959

13 Short Take-Off and Landing Jet Plane Fitted with a “Compound Propulsion System” FIAT

Sep 16 1959

14 AFFDL-TR-71-26-VOL I STOL High-Lift Design Study Volume I. State of the Art Review of STOL Aerodynamic Technology

Apr 1971

15 NASA CR 114612 Quiet Turbofan STOL Aircraft for Short Haul Transportation – Final Report Contract# NAS 2-6995 Lockheed

Jun 14 1973

16 NASA CR 114613 Quiet Turbofan STOL Aircraft for Short Haul Transportation – Final Report Contract# NAS 2-6995 Lockheed

Jun 14 1973

17 NASA CR-(?) Study of Quiet Turbofan Aircraft for Short Haul Transportation Lockheed

Jul 1973

18 MDC-J4371 Study of Quiet Turbofan STOL Aircraft for Short-Haul Transportation – Final Report – Volume I : Summary Contract# NAS2-6994 Lockheed

Jun 1973

19 MDC-J4371 Study of Quiet Turbofan STOL Aircraft for Short-Haul Transportation – Final Report – Volume II : Aircraft Contract# NAS2-6994 Lockheed

Jun 1973

20 MDC-J4371 Study of Quiet Turbofan STOL Aircraft for Short-Haul Transportation – Final Report – Volume III : Airports Contract# NAS2-6994 Lockheed

Jun 1973

21 MDC-J4371 Study of Quiet Turbofan STOL Aircraft for Short-Haul Transportation – Final Report – Volume IV : Markets Contract# NAS2-6994 Lockheed

Jun 1973

22 MDC-J4371 Study of Quiet Turbofan STOL Aircraft for Short-Haul Transportation – Final Report – Volume V : Economics Contract# NAS2-6994 Lockheed

Jun 1973

23 MDC-J4371 Study of Quiet Turbofan STOL Aircraft for Short-Haul Transportation – Final Report – Volume VI : Systems Analysis Contract# NAS2-6994 Lockheed

Jun 1973

TRI-SERVICE TRANSPORT- D-828 (DOUGLAS REPORT ES40292 )

60 1 Douglas Proposal Sketches and Loose Papers for ES 40292 Mar 31 1961 2 ES 40292 Features of the D-828 Concept Douglas Apr 12 1961 3 ES 40292 Book 1 Program General Summary (Lots I and Mar 31 1961

127

II) Douglas 4 ES 40292 Book 2 Summary Report (Technical) Douglas Mar 31 1961 5 ES 40292 Book 3 Operational Suitability Douglas Mar 31 1961 6 ES 40292 Book 4 Configuration Selection Douglas Mar 31 1961 7 ES 40292 Book 5 Effects of Dimensional Limitations

Douglas Mar 31 1961

8 ES 40292 Book 7 Part II Power Plant Analysis Douglas Mar 31 1961 9 ES 40292 Book 9 Aerodynamic Test Program Douglas Mar 31 1961 10 ES 40292 Book 10 Part I Weight and Balance Douglas Mar 31 1961 11 ES 40292 Book 10 Part II Weight and Balance Douglas Mar 31 1961 12 ES 40292 Book 11 Structural Description and Design Data

Douglas Mar 31 1961

13 ES 40292 Book 12 Structural Test Program Douglas Mar 31 1961 14 ES 40292 Book 13 Flight Control Systems Douglas Mar 31 1961 15 ES 40292 Book 14 Power Plant Installation and Fuel

System Douglas Mar 31 1961

16 ES 40292 Book 14 Appendix D Hamilton Standard Propellers Douglas

Mar 31 1961

17 ES 40292 Book 14 Appendix E Development Status of Variable Camber Propeller Douglas

Feb 15 1961

18 ES 40292 Book 14 Appendix F Propeller Fiberglass Blade Construction Douglas

Mar 31 1961

19 ES 40292 Book 14 Appendix G Power Plant Main Transmission Gearbox Douglas

Mar 31 1961

20 ES 40292 Book 15 Hydraulic and Landing Gear Systems Douglas

Mar 31 1961

21 ES 40292 Book 16 Electrical Systems Douglas Mar 31 1961 22 ES 40292 Book 17 Instruments and Avionics Systems

Douglas Mar 31 1961

23 ES 40292 Book 18 Crew and Cargo Compartments Douglas

Mar 31 1961

24 ES 40292 Book 19 Detail Specifications Douglas Mar 31 1961 25 ES 40292 Book 20 Demonstration Program Douglas Mar 31 1961 26 ES 40292 Book 21 Maintenance and Support Douglas Mar 31 1961 27 ES 40292 Book 22 Program Plan – Schedules,

Management and Resources Douglas Mar 31 1961

28 ES 40292 Book 22 Appendix C Cost reductions in Navy Programs Douglas

Mar 31 1961

29 ES 40292 Book 23 Cost and Contract Terms Douglas Mar 31 1961 30 ES 40292 Book 24 Lot III Program Douglas Mar 31 1961 31 Addendum No. 104A (Proposed) to Specification MIL-D­

8706(AER)-2 Design Data and Tests Lot I Douglas Apr 15 1961

32 Addendum No. 104B (Proposed) to Specification MIL-D­8706(AER)-2 Design Data and Tests Lot II Douglas

Apr 15 1961

Tri-Service VTOL Transport Aircraft - North

128

American Aviation, Inc Document NA61H 61 1 -102 Technical Summary Apr 3 1961

2 -103 Detail Specification Apr 3 1961 3 -104 Master Development Plan Apr 3 1961 4 -105 Technical Development Plan Apr 3 1961 5 -106 Weight and Balance Apr 3 1961 6 -108 Stability and Control Analysis Apr 3 1961 7 -110 Electrical System Apr 3 1961 8 -111 Structural Description and Design Data Apr 3 1961 9 -113 Power Plant Installation and Fuel System Apr 3 1961 10 -114 Hydraulic and Pneumatic Systems Apr 3 1961 11 -115 Maintenance and Support Apr 3 1961 12 -116 General Demonstration Requirements for Tri-Service

VTOL Apr 3 1961

13 -117 Design Analysis and Effects of Dimensional Limitations

Apr 3 1961

14 -118 Reliability and Value Control Apr 3 1961 15 -119 Human Factors Engineering Apr 3 1961 16 -120 Control Systems Apr 3 1961 17 -121 Simulation Study of Hovering and Transition Flight Apr 3 1961 18 -122 Statement of Work Apr 3 1961 19 -123 Electronic System Apr 3 1961 20 -125 Estimated Moments of Inertia Apr 3 1961 21 -126 Tilt-Wing Dynamic Development Vehicle Apr 3 1961 22 -128 Modified Program Statement of Work Apr 3 1961 23 -127 Program Management Report Apr 3 1961 24 -193 Low Speed Wind Tunnel Tests on a .165-scale Full

Span Model of a V/STOL Vehicle to Determine Aerodynamic Characteristics in Transition and Hovering Flight

Apr 3 1961

25 -213 Low Speed Wind Tunnel Tests on a .165-scale Four Engine Tilt Wing Model of a V/STOL Vehicle to Determine Aerodynamic Characteristics in Transition and Hovering Flight

Apr 3 1961

SR-175 (BELL) & DUCTED PROPELLER 62 1 Report No. D181-945-002 Ducted Propeller Assault

Transport Design Report Contract# Nonr-1675(00) May 15 1956

2 Report No. D181-945-003 Ducted Propeller Assault Transport Survey-State of the Art Contract# Nonr­1675(00)

May 15 1956

3 Report No. D181-945-004 Ducted Propeller Assault Transport Performance Contract# Nonr-1675(00)

May 15 1956

4 Report No. D181-945-006 Ducted Propeller Assault Transport Duct and Propeller Analysis Contract# Nonr­1675(00)

May 15 1956

129

5 NASA TN D-4343 Wind-Tunnel Investigation of Lateral Aerodynamic Characteristics of a Powered Four-Duct-Propeller VTOL Model in Transition

Feb 1968

6 Report No. 2-60-945001 SR-175 VTOL/STOL Logistics Aircraft Parameter Study Bell Aircraft Corp.

Feb 29 1960

7 Report No. D190B-945-008 V/STOL Interim Transport Aircraft Weapons System Analysis Report Bell Aircraft Corp.

Jul 10 1959

8 Report No. D190B-945-009 V/STOL Interim Transport Aircraft Detail Specification Report Bell

Jul 10 1959

9 Report No. D190B-945-010 V/STOL Interim Transport Aircraft Aerodynamics Data Bell

Jul 10 1959

10 Report No. D190B-945-011 V/STOL Interim Transport Aircraft Structural Report Bell

Jul 10 1959

11 Report No. D190B-945-012 V/STOL Interim Transport Aircraft Weight and Balance Report Bell

Jul 10 1959

12 Report No. D190B-945-014 V/STOL Interim Transport Aircraft Stability and Control – Hovering and Transition Bell

Jul 10 1959

13 Report No. D190B-945-015 V/STOL Interim Transport Aircraft Propulsion System Analysis Bell

Jul 10 1959

14 Report No. D190B-945-016 V/STOL Interim Transport Aircraft Electrical System Load Analysis

Jul 10 1959

15 Report No. D190B-945-018 V/STOL Interim Transport Aircraft Technical Summary Bell

Jul 10 1959

16 Report No. D190B-945-020 V/STOL Interim Transport Aircraft for Air Recovery Liaison General Utility Bell

Aug 1959

17 Report No. D190B-945-022 V/STOL Interim Transport Aircraft for Air Recovery Liaison General Utility Bell

Nov 1960

TRI-SERVICE TRANSPORT -BELL/LOCKHEED 63 1 Report No. D2064-953001 Tri-Service VTOL Transport

Volume 1 Part II Technical Summary Bell & Lockheed Apr 1961

2 Report No. D2064-953001 Tri-Service VTOL Transport Volume 2 Detail Specification Bell & Lockheed

Apr 1961

3 Report No. D2064-953001 Tri-Service VTOL Transport Volume 3 Weight and Balance Bell & Lockheed

Apr 1961

4 Report No. D2064-953001 Tri-Service VTOL Transport Volume 4 Power Plant Analysis Bell & Lockheed

Apr 1961

5 Report No. D2064-953001 Tri-Service VTOL Transport Volume 6 Standard Aircraft Characteristics Charts Bell & Lockheed

Apr 1961

6 Report No. D2064-953001 Tri-Service VTOL Transport Volume 7 Stability and Control Bell & Lockheed

Apr 1961

ACADEMIC VTOL & AHS PROCEEDINGS

130

5

10 15

20

25

64 1 IAS Annual Meeting – A Tested Solution of the Problem of Helicopter Stability and Automatic Control by Donald N. Meyets & Edward G. Vanderlip Piasecki & P. Halpert Sperry Gyroscope

Jan 29 1951

2 Report D6-5201 SR-175 Program Study Boeing Jan 1960 3 Report ER-4221 (60WCL-675) SR-175 V/STOL Logistic

Aircraft Parametric Study 1965-1970 Time frame Collection of Pertinent Data Lockheed-Georgia

Feb 1 1960

4 Report 60WWR-930 SR-175 V/STOL Logistic Aircraft Study Summary and Recommendations

Jun 23 1960

VTOL-STOL Hazards and Special Problems Conference Jan 26 1961 6 Report TOR-0073(3657-01)-1 Equipment Systems

Improvement Program – Development Evaluation of Aerial Vehicles for Law Enforcement Applications by J.B. Nichols Contract# F04701-72-C-0073

Jun 1973

7 1st Convertible Aircraft Congress Proceedings Dec 9 1949 8 2nd Convertible Aircraft Congress Proceedings Dec 12 1952 9 3rd Convertible Aircraft Congress Proceedings Nov 25 1955

4th Convertible Aircraft Congress Proceedings 1958 11 Proceedings of the Third Annual Forum of the AHS Mar 27-29 1947 12 Proceedings of the Fifth Annual Forum of the AHS May 12-13 1949 13 Proceedings of the Eleventh Annual Forum of the AHS Apr 27-30 1955 14 Proceedings of the Thirteenth Annual Forum of the AHS May 8-11 1957

Proceedings of the Eighteenth Annual Forum of the AHS May 2-4 1962 16 Proceedings of the Nineteenth Annual Forum of the AHS May 1-3 1963 17 AHS 28th Annual Forum – Presentations and Index May 1972 18 R & D Contributions to Aviation Progress (RADCAP)

Volume I Summary Report Aug 1972

19 R & D Contributions to Aviation Progress (RADCAP) Executive Summary

Aug 1972

Gothert’s Report – VTOL Sections Undated 21 VTOL Technology for Systems Undated 22 Some Thoughts on the Design Philosophy of Subsonic

VTOL Transports by W.Z.Stepniewski Boeing-Vertol Dec 16 1960

23 Looking Ahead in V/STOL by George S. Schairer Sep 1961 24 Lecture Notes from a Short Course in V/STOL Univ. of

Tenn. Space Inst. Nov 18-23 1968

Proceedings of the Experimental V/STOL Aircraft Lessons Learned Sessions of the AIAA/AHS/ASEE Aircraft Design, Systems, and Operations Meeting

Sep 17-19 1990

VTOL TRANSPORTS 65 1 AFFDL-TR-66-195-Volume I The X-19 V/STOL

Technology – A Critical Review ( 2 copies) May 1967

2 Wind Tunnel Report 1005 X-200 Turbine Stability Model Curtiss MIT

Nov 7 1960 to Nov 23 1960

131

3 Wind Tunnel Report 1005 X-200 Turbine Stability Model Curtiss MIT

Jan 16 1961 to Feb 1 1961

4 Report No. 014-544 50-Hour Qualification Test X-19 Propeller Control Coordinator and SAS Assembly Vol. I Curtiss

Oct 25 1965

5 Report No. 030-37 Curtiss-Wright Model 207-8 V/STOL Multi-Mission Support Transport

Sep 19 1965

6 Concept Sketches Curtiss-Wright VTOL Model X-19 C.A. 1965 7 Report SD-139 Curtiss-Wright High-Speed VTOL

Airplane Model 200 General Configuration and Performance

Aug 1960

8 Report VS-118 Comparative Data X-19 Light Utility VTOL Transport

Sep 1964

9 Report No. 200-100 Model Specification Curtiss-Wright Model 200 High Speed VTOL Transport

Feb 15 1961

10 Report PDA 893063 Model 260-7 USAF Multi-Mission (RVX) Aircraft Design Study Curtiss

Aug 30 1963

11 Report VS-112 VTOL Transport Data Based on Preliminary Design Studies Curtiss

Sep 1963

12 Report PDA 10163 Model 203 Light Utility Transport Curtiss

Oct 1 1963

13 AFFDL-TR-66-195-Volume II The X-19 V/STOL Technology – A Critical Review ( 2 copies)

May 1967

14 X-19 Material 1961-1965 15 Evaluation of Curtiss-Wright VTOL Aircraft Programs 1961 16 Dornier DO-29 1960 17 Curtiss-Wright Blueprints 1961 18 Report 200-5.1.0.1 X-19 Landing Loads Criteria Dec 18 1963 19 Curtiss-Wright X-19 Papers 1963

TRI-SERVICE TRANSPORT, ADAM PROGRAM 66 1 NACA TN D-89 Wind-Tunnel and Piloted Flight

Simulator Investigation of a Deflected-Slipstream VTOL Airplane, the Ryan VZ-3RY

C.A. 1958

2 NACA TN 3182 Manual of the ICAO Standard Atmosphere

May 1954

3 Relative Power Requirement Under Static Condition Between the Tilt-Wing-Propeller and Deflected Slipstream VTOL Aircraft by Harlan D. Fowler with Letter to Lindenbaum

Aug 8 1963

4 Fowler Draguration Flap System 1964 5 Harlan D. Fowler Letters 1959-1965 6 Report RAC-1012 Variable Sweep Wing Plus V/STOL –

A New Era in Aircraft Design – Part I – Aerodynamic Design Concepts Republic

Dec 12 1962

7 Report RAC-1012 Variable Sweep Wing Plus V/STOL – Dec 12 1962

132

A New Era in Aircraft Design – Part II – Takeoff and Landing Performance Republic

8 Photos, Clippings of Deflected Slipstream A/C & Prop. STOL

Various

9 Report D3-3900-18 Boeing Model 900 Tri-Service VTOL Prototype Transport

Apr 2 1961

10 Report D3-3900-16 Proposal for a Tri-Service VTOL Prototype Transport Aircraft

Apr 17 1961

11 Report D3-3900-17 Proposal for a Tri-Service VTOL Prototype Transport Aircraft – Price Analysis

Apr 3 1961

12 AIAA Paper No. 69-201 The ADAM III V/STOL Concept by Byron R. Winborn, Jr. LTV

Feb 17-19 1969

13 ADAM (Air Deflection and Modulation) Vought Undated 14 ADAM II LTV Undated

15 The Evolution of the ADAM Concept by B.R. Winborn Vought

Jul 11 1968

16 Report No. EOR-12684 ADAM Air Force Transport Study SR 175

Feb 12 1960

17 ADAM notes and Photos Undated 18 Appraisal of Comparative Evaluation – Fan-in-Wing

Versus ADAM II Jan 10 1964

19 Report No. 2-55300/2R428 ADAM II Test Program Proposal Chance-Vought

Dec 12 1962

20 ADAM II Blueprint and Specifications Undated 21 Report AER-EOR-12725 Low Speed Wind-Tunnel Tests

of a 0.15 Scale Model “ADAM” VTOL Airplane Series I & II

Mar 8 1960

22 ADAM II Ten Ton Transport LTV Correspondence Oct 21 1964 23 Comparative Evaluation of the Fan-In-Wing and ADAM II

V/STOL Surveillance Airplanes LTV Jan 1964

24 AFFDL-TR-68-31 Part II Design, Fabrication, Testing, and Data Analysis of ADAM II Concept Part II, Shakedown Testing on Vought Aeronautics Division 7ft x 10ft Low Speed Wind Tunnel

May 1968

25 AFFDL-TR-68-31 Part III Design, Fabrication, Testing, and Data Analysis of ADAM II Concept Part III, Testing in 17ft Test Section of 7ft x 10ft Wind Tunnel, NASA Langley

May 1968

26 AFFDL-TR-68-31 Part IV Design, Fabrication, Testing, and Data Analysis of ADAM II Concept Part IV, Testing in the Langley Center 16-foot Transonic Wind Tunnel

May 1968

27 Report No. 2-53310/4R-2166 Analysis of a Low Speed Wind Tunnel Test of a High Mass Vectored Propulsion Flow Model Contract DA-31-124-ARO-D-262 LTV

Feb 15 1965

28 Report No. 2-53310/4R-2206 Analysis of a Follow-On Jul 31 1965

133

Low Speed Wind Tunnel Test of a High Mass Vectored Propulsion Flow Model Contract DA-31-124-ARO-D-262 LTV

29 Report No. 2-55400-50309 An Investigation of the Effect of Fan-Generated Turbulence on Flows in Ducts, Diffusers, and Bends LTV

Aug 19 1965

30 Report No. 2-55400-50331 Planning Document – ADAM II Experimental Program LTV

Jan 17 1966

31 Report No. 2-55400-50331 Planning Document – ADAM II Experimental Program Annex I: Estimated Costs

Jan 17 1966

32 ADAM II Hi/Lo Model Undated 33 ADAM Blueprints Various 34 “DISCOJET” Proposal M Research 1969-1970 35 A VTOL Airplane for Commercial Uses Allison 250 HP

by Harlan D. Fowler Nov 10 1960

36 V/STOL Commercial Transport 18 Passengers or 5000 lbs. Cargo Model 70 by Harlan D. Fowler

Nov 18 1964

37 Progress Report No. 25 Model M-224I STOL/VTOL Test Vehicle Contract# DA 44-177-TC-350 Fairchild

Mar 31 1958

SR-175, VTOL TRANSPORTS 67 1 Computed Induced Velocity, Induced Drag, and Angle of

Attack Distributions for a Two-Bladed Rotor by Raymond Piziali & Frank DuWaldt Cornell Contract# DA 44-111­TC-698

C.A. 1962

2 YAK-36 & “Freehand” Photos & Articles 1976 3 Flight Test Experiences in Obtaining the First Commercial

Certification of a Helicopter for True Vertical Flight Takeoff and Landing Capability by John Diamond, Herbert H. Moser & Philip Camerano Boeing-Vertol

Undated

4 Miscellaneous Photos – STOL Aircraft Various 5 The Joint Army Navy Aircraft Instrument Research

Program Status Report by Harry W. Mitchel Bell May 1-3 1963

6 US/FRG V/STOL Technology Review May 6-7 1969 7 Report No. 2127-950011 X-22A Tri-Service Dual Tandem

Ducted Propeller VSTOL Aircraft Bell Jan 1968

8 Model 2064 Blueprints Bell – Lockheed Mar 1961 9 AHS 27th Annual V/STOL Forum Paper No. 544 Factors

Affecting Handling Qualities of a Lift-Fan Aircraft During Steep Terminal Area Approaches by Ronald M. Gerdes & Charles S. Hynes Ames Research Center

May 1971

10 Hummingbird Derivatives – “Centerline Lift” VTOL Aircraft Design Approach Lockheed-Georgia

Nov 1964

11 Ejector Thrust Augmentor Various 12 Dornier AG Dornier System GmbH Information Packet Feb 1970 13 VAK 191B Articles and Photos C.A. 1966

134

14 VTOL Transporters Vereinigte Flugtechnische Werke VFW (in German)

Undated

15 Report 60WWR-930 SR-175 V/STOL Logistics Aircraft Study Summary and Recommendations

Undated

16 Report ER-4221 SR-175 V/STOL Parametric Study 1965­1970 Time Frame Lockheed-Georgia

Feb 1 1960

17 Report SER-50107(Part II) SR-175 VTOL/STOL Logistics Aircraft Part 2 – Mission B – Design Study Sikorsky

Apr 26 1960

18 Review of Lockheed Type A V/STOL Design by B. Lindenbaum

Nov 14 1977

19 Report SER-50107(Part I) SR-175 VTOL/STOL Logistics Aircraft Part 1 – Mission A – Design Study Sikorsky

Mar 21 1960

20 Report R-294 Summary Presentation – USAF SR-175 VTOL/STOL Logistics Aircraft Parametric Study 1965­1970 Time Frame Kaman

Apr 8 1960

21 Report D6-15362 Flight into the Atmosphere, 1975-1985 With Presentation Handout Boeing

May 16 1966

22 Report H034 Research in Advanced Technology for Naval Vertical Lift Aircraft Final Report Contract# N00014-68­C-0441

Mar 15 1969

23 Part C. Technical Possibilities & Technical Program (incomplete)

Undated

24 AIAA-83-2491 On Overview of V/STOL Aircraft Development by S.B. Anderson NASA Ames

Oct 17-19 1983

25 IAS 26th Annual Paper 808 Research in the Field of Wingless VTOL Aircraft by A.M. Lippisch Collins Radio

Jan 27-30 1958

26 IAS Summer Meeting Paper 59-122 Design Philosophy and Test Experiences of a VTOL Aircraft by Bruno J. Uberti & James B. Reichert Doak

Jun 16-19 1959

27 IAS Summer Meeting Paper 59-123 Lifting Systems for VTOL Vehicles by Scott Rethorst & W.W. Royce VRC

Jun 16-19 1959

28 AHS 95-2.5-1-9 Similarly Configured Public Use Vertical Airports for VSTOL Commuter Aircraft by William F. Chana Chana Assoc. & John B. Adams JAG Architecture

Jan 18-20 1995

29 VTOL Transportation for 1985 Presentation Handout Undated 30 Status of STAMP/STARS-V Development Program

Presentation Handout Hydra-Electric Co. Jul 9 1973

31 Performance Possibilities of Subsonic Airplanes Taking Off and Landing on the Ground Cushion by W.Z. Stepniewski Vertol

Oct 21-23 1959

32 ASTOVL – A New Look at Airbase Independence Presentation Handout McDonnell Douglas

Oct 21 1986

33 Limited Flight Experience with Several Types of VTOL Aircraft by John P. Reeder & Fred J. Drinkwater III NASA

Feb 1960

34 Fiat G91 Successor Sketches Undated

135

35 Miscellaneous Copies Undated 36 Mass Transportation – A Systems Concept by F.H.

Furguson Advanced Concepts Feb 1968

37 Report ER 9766 Mass Air Transportation Study Final Report Lockheed-Georgia

Apr 1968

38 R. & M. No. 3263 Measurement of Lift and Ground Interference on a Lifting-Fan Wing at Zero Forward Air Speed

1962

39 SAE 221 Some Performance and Operating Characteristics of Convertiplanes by R.L. Lichten Bell Helicopter

Sep 30-Oct 5 1957

40 NASA TN – D-56, D-372(2), D-444, D445, D513(2), D­616, D720, D-733, D-756, D-785, D-1233

1959-1962

41 NACA TN – 3692, 3904, 4181 1956-1957

V/STOL, SR-175 68 1 V/STOL Photos and Miscellaneous Articles Various

2 AHS Eastern Regional meeting – The Convertiplane by Col. William B. Bunker US Army

Jun 8 1954

3 Report No. N79-10024 Study of Aerodynamic Technology for VSTOL Fighter/Attack Aircraft-Horizontal Attitude Concept by S.H. Brown Northrop

May 1978

4 Summary of Recent Vought V/STOL Studies Feb 12 1980 5 Report No. AFWAL-TR-86-3071 Volume I – V/STOL

Concepts and Developed Aircraft Volume I – A Historical Report (1940-1986) by B. Lindenbaum

Nov 1986

6 CAD/Vertol Commercial V/STOL System Analysis – Technical Review Minutes Boeing

Feb 20-22 1967

7 Report No. DM-62-14 A Comparison of VTOL Propulsion Systems in a Subsonic Mission by W.L. Rodenbaugh GE

Jan 18 1962

8 The Convertiplane – Implications of a New Aircraft Type on the National Aviation Policy of the US.

Oct 1954

9 Convertiplane Interest Grows Fast by Robert McLarren from Aviation Week

Dec 26 1949

10 Some Aspects of Convertible Aircraft Design by Robert L. Lichten Bell

May 9 1949

11 NASA Conference on V/STOL Aircraft Nov 17-19 1960 12 NASA SP-116 Conference on V/STOL and STOL Aircraft Apr 4-5 1966 13 Presentation to NASA Advisory Committee on Aircraft

Propulsion May 3-4 1967

14 Report No. PR69-ATT-999 Low Speed Thrust Reverser Technology

May 29 1969

15 Mach 2 V/STOL (VJ 101) Flight Test Program by George L. Bright

Sep 27-28 1963

16 High Speed VTOL Transports Undated 17 Avenues for Research 1966 US Army Aviation Materials Jun 1966

136

Lab. by Henry R. Velkoff 18 Text of Presentation to Aircraft Working Group – USAF

Scientific Advisory Board Nov 1964

19 VTOL/STOL – Aircraft Bibliography Mar 31 1961 20 Report NO. SER-50112 USAF SR 175 VTOL STOL

Aircraft Survey Sikorsky Aug 19 1960

21 Report No. 60WWR-930 SR-175 V/STOL Logistic Aircraft Study Vol. I Appendix Contractor Report Summaries

Jun 1960

22 Looking Ahead in V/STOL by George S. Schairer Sep 1961 23 Report No. FDCC TM 66-11 Research Requirements for

V/STOL Gust Response and Low Altitude Turbulence Model

Oct 1966

24 Report No. AGARDograph 46 Symposium on Vertical & Short Take-Off and Landing Aircraft Part I

Jun 1960

25 AFFDL-TR-68-85 Investigation of the Effects of Gusts on V/STOL Craft in Transition and Hover

Oct 1968

26 USAAVLABS TR 69-13 Review and Preliminary Evaluation of Lifting Horizontal-Axis Rotating-Wing Aeronautical Systems (HARWAS) Contract# DAAJ02-67­C-0046

Mar 1969

27 USAAVLABS TR 69-14 A Study of Aerodynamic Performance Evaluation and Comparison Techniques for V/STOL Aircraft Contract# DA 44-177-AMC-376(T)

Jul 1969

28 ASD-TR-69-15 Part II Propeller Static Performance tests for V/STOL Aircraft Part II. Test Data (Appendix III)

Jan 1970

29 Report No. SURVIAC-TR-91-008 V/STOL Compendium and Database

Dec 1990

TRI-SERVICE TRANSPORT - BELL / LOCKHEED VTOL Proposal + WADC 59-21 + WADC 58-96to99

69 1 Report No. D2064-953001 Volume 8 Structural Description and Design Data

Apr 1961

2 Report No. D2064-953001 Volume 9 Power Plant Installation and Fuel System

Apr 1961

3 Report No. D2064-953001 Volume 13 Demonstration Program

Apr 1961

4 Report No. D2064-953001 Volume 15 Effects of Dimensional Limitations

Apr 1961

5 Report No. D2064-953001 Volume 18 Wind Tunnel Test Data

Apr 1961

6 Report No. D2064-953001 Volume 19 Propeller and Gearbox Design

Apr 1961

7 WADC TR No. 59-21 Part I A Study of the Feasibility of Using a Semi-Rigid or Fully Articulated Rotor on a Tilt-

Nov 12 1958

137

Wing Type Vertical Takeoff and Landing Aircraft – Final TR – Part I Containing: Summary of Study Bell report D232-099-009 Contract# AF 33(616)-5089

8 WADC TR No. 59-21 Part II A Study of the Feasibility of Using a Semi-Rigid or Fully Articulated Rotor on a Tilt-Wing Type Vertical Takeoff and Landing Aircraft – Final TR – Part II Containing: Bell Reports D232-099-001, 003, 004 Vol I Contract# AF 33(616)-5089

Nov 1 1957

9 WADC TR No. 59-21 Part III A Study of the Feasibility of Using a Semi-Rigid or Fully Articulated Rotor on a Tilt-Wing Type Vertical Takeoff and Landing Aircraft – Final TR – Part III Containing Bell Reports D232-099-004 Vol II Contract# AF 33(616)-5089

Nov 12 1957 rev Mar 28 1958

10 WADC TR No. 59-21 Part IV A Study of the Feasibility of Using a Semi-Rigid or Fully Articulated Rotor on a Tilt-Wing Type Vertical Takeoff and Landing Aircraft – Final TR – Part IV Containing Bell Report D232-099-001 Vol III Contract# AF 33(616)-5089

Nov 12 1957 rev Mar 28 1958

11 WADC TR No. 59-21 Part VI A Study of the Feasibility of Using a Semi-Rigid or Fully Articulated Rotor on a Tilt-Wing Type Vertical Takeoff and Landing Aircraft – Final TR – Part VI Containing Bell report D232-099-002, 005, 006, 008 Contract# AF 33(616)-5089

Nov 12 1957

12 WADC TR No. 59-21 Part VII A Study of the Feasibility of Using a Semi-Rigid or Fully Articulated Rotor on a Tilt-Wing Type Vertical Takeoff and Landing Aircraft – Final TR – Part VII Containing Bell Report D232-099-007, 010 Contract# AF 33(616)-5089

Nov 11 1957

13 WADC TR 58-96 STOL/VTOL Propeller Study Contract# AF 33(600)-35021 Vertol

Mar 1958

14 WADC TR 58-97 STOL/VTOL Propeller Study – Aerodynamic Analysis Contract# AF 33(600)-35021 Vertol.

Mar 1958

15 WADC TR 58-98 STOL/VTOL Propeller Study – Aero-Elastic Vibration Analysis Contract# AF 33(600)-35021 Vertol

Mar 1958

16 WADC TR 58-98 STOL/VTOL Propeller Study – Stress and Weight Analysis Contract# AF 33(600)-35021 Vertol

Mar 1958

17 Report No. R351-001 M-351 Proposed Low Speed System Investigation for Tri-Service VTOL Assault Transport Fairchild

Apr 3 1961

SR-175 - BELL X-22A & SHROUDED PROPELER 70 1 Report No. D181-945-001 Ducted Propeller Assault

Transport – Summary Report Contract# Nonr-1675(00) May 15 1956

138

Bell 2 Report No. D181-945-005 Ducted Propeller Assault

Transport – Stability and Control Contract# Nonr­1675(00) Bell

May 15 1956

3 Report No. D181-945-006 Ducted Propeller Assault Transport – Duct and Propeller Analysis Contract# Nonr­1675(00) Bell

May 15 1956

4 Report No. D181-945-007 Ducted Propeller Assault Transport – Preliminary Structural Analysis Contract# Nonr-1675(00) Bell

May 15 1956

5 Report No. 2127-933009 X-22A Progress Report No. 9 Contract# Now 63-0118-ci Bell

Sep 15 1963

6 Report No. 2127-933073 X-22A Progress Report No. 73 Final Contract# Now 63-0118-ci Bell

Apr-Dec 1969

7 Report No. 2-60-945001 SR-175 VTOL/STOL Logistics Aircraft Parametric Study Bell

Feb 29 1960

8 IAS Report No. 59-59 Research Studies on the Ducted fan Equipped with Turning Vanes by A.W. Gilmore & W.E. Grahame Grumman

Jan 26-29 1959

9 Report No. 2127-917003 Aerodynamic Stability and Control and Flying Qualities, X-22A Contract# Now 63­0118-ci Bell

Dec 28 1962

10 X-22A Miscellaneous Various 11 Report No. 2127-950012 Interim Flight Test

Accomplishments – X-22A Bell Mar 1966 – Feb 1969

12 Report No. 2127-917006 Performance Data Report X-22A Contract# Now 63-0118-ci Bell

Apr 1 1963

13 Report No. D2038-953001 Appendix – Analytical Evaluation and Design of Ducted Propellers

Jul 6 1960

14 Report No. 2-60-945003 Summary of Bell Ducted Propeller

Dec 1960

15 Report No. 2-59-920002 Ducted Propeller Test Stand – Description Bell

Dec 1959

16 Report No. 59-A-3 Stability and Control Analysis – PiAC 59H – Aerial Jeep VZ-8P-II Contract# DA 44-177-TC-449 Piasecki

Feb 24 1962

17 Report No. 59-X-30 Piasecki AIRGEEP Vehicles for Army Tactical Mobility Requirements Board

Jun 15 1962

18 Report No. GDC PIN 68-805 A Proposal Wind Tunnel Test Program for Full-Scale, Single-Place Stacked Rotor Volume I – Technical General Dynamics

Oct 1968

19 Report No. R221-012 Compressibility Effect on a Shrouded Propeller Fairchild

Nov 1955

20 AIAA Paper No. 68-994 Shrouded Propellers – A Comprehensive Performance Study by Donald M. Black & Harry S. Wainauski & Carl Rohrbach United Aircraft

Oct 21-24 1968

139

21 SAE No. 730323 Shrouded Fan Propulsors for Light Aircraft

Apr 3-6 1973

22 IAS No. 621 An Application of the Ducted Propeller to a VTOL Transport Aircraft by James A. O’Malley, Jr. Bell

Jan 23-26 1956

23 NACA TR 3547 Aerodynamic Characteristics of a Small-Scale Shrouded Propeller at Angles of Attack from 0o to 90o

Nov 1955

24 Aero Report 904 Approximate Calculation of the Shrouded Propeller

Jul 1956

25 NASA TN D-995 Aerodynamic Loads on an Isolated Shrouded-Propeller Configuration for Angles of Attack from -15o to 110o

Jan 1962

26 NASA TN D-4142 A Wind-Tunnel Investigation of a 7­foot-Diameter Ducted Propeller

Aug 1967

27 FTD-HT-66-273 Applications of Ducted-Fan Propellers in the Ground Forces by J. Soulez-Lariviere (from French)

Oct 14 1966

28 Progress Report No. 10 Two-Ducted Aerial Research Vehicle Period May 1 to May 31 Contract# DA-44-177­TC-448

Jun 5 1958

29 Progress Report No. 11 Two-Ducted Aerial Research Vehicle Period Jun1 to Jun 30 Contract# DA-44-177-TC­448

Jul 7 1958

30 Progress Report No. 12 Two-Ducted Aerial Research Vehicle Period Jul 1 to Jul 31 Contract# DA-44-177-TC­448

Aug 5 1958

31 Report No. 149 Ducted Propeller Weight Lifter Contract Nonr 2199(00) Hiller

Nov 22 1957

TILT-WING V/STOL, CL-84,X-18,VC 400, XC-142A 71 1 AIAA No. 63-484 The Aerodynamic Approach to

Improved Flying Qualities of Tilt-Wing Aircraft by J.F. Martin & O.E. Michaelsen Canadair

Oct 21-24 1963

2 AIAA 90-3204 The LTV XC-142 Experimental Aircraft Lessons Learned by George E. Dausman US Army

Sep 17-19 1990

3 CL-84 Assorted Papers and Photos Canadair Various 4 Tilting Propeller Aircraft – Clippings and Photos Various 5 X-18/19 Photos and Articles 1990 6 Surveillance Aircraft System ASR No. 2-60 Martin Co. Dec 1 1959 7 Report No. R-183 A Proposal for the Design, Construction

& Test of the K-16B VTOL/STOL Research Vehicle Kaman

Nov 6 1957

8 VC 400 VTOL Cargo Aircraft VFW Munich Jun 1966 9 VC 400 Design and Operational Capability VFW Munich Apr 19 1968 10 VC 500 Briefing VFW Munich Dec 13 1969

140

11 VC 400 Articles and Brochures Various 12 Ishida Group Tilt-Wing Proposal Papers 1999 13 Report No. R-284 Shrike, ASR 2-60 Kaman Jan 29 1960 14 VZ-2 Papers Undated 15 The Canadair V/STOL Aircraft Program Nov 11 1963 16 Report No. ERR-CL-RAX-84-118 A Study of Cyclic Pitch

Propeller Application to the CL-84 Tilt Wing V/STOL Prototype Hydro/Aero/Astronautical Sciences Canadair

Oct 1965

17 Report No. RAX-84-121 CL-84G Search and Rescue Variant Canadair

Nov 29 1965

18 Report No. RAX-84-128 Technical Proposal for a Cyclic Pitch Propeller Development and Testing Program Canadair

Apr 1966

19 CL-84-1D Operational Evaluation Study for the USAF Canadair

Sep 1969

20 XC-142A V/STOL Transport Brochure Hiller, Vought, Ryan

Undated

21 NASA TN D-535 Damage Incurred on aTilt-Wing Multipropeller VTOL/STOL Aircraft Operating Over a Level, Gravel-Covered Surface

Dec 1960

22 USAAVLABS TR 67-84 Tri-Service Evaluation of the Canadair CL-84 Tilt-Wing V/STOL Aircraft

1967

23 Report No. 503 Application of Small-Scale Propeller Test Data to V/STOL Aircraft Design by Henry E. Payne III Princeton Univ.

Oct 1961

24 USAAVLABS TR 66-64 Comparison of Longitudinal Stability Characteristics of three Tilt-Wing VTOL Aircraft Designs Contract# DA 44-177-AMC-8(T)

Jan 1968

25 V/STOL’s Time Has Come by Edgar E. Ulsamer Air Force/Space Digest

Oct 1969

26 VC 400 Brochure VFW Munich Undated 27 XC-142A Lessons Learned Papers 1966 28 History of XC-142A Tri-Service Program 1967 29 NASA TN D-4344 Calculation of the Dynamic

Longitudinal Stability of a Tilt-Wing V/STOL Aircraft and Correlation with Model Test Flights

Feb 1968

30 Initial Development and Testing of a Tilt-Wing V/STOL by W.S. Longhurst Canadair

Undated

31 Potential Propeller Technology and Static Thrust Augmentation by George Rosen

May 17 1966

32 Royal Aero Society Volume 67 No. 630 Development of the Tilt-Wing Aircraft by John B. Nichols Hiller

Jun 1963

33 Vietnam/C-142 “What Can BE” Brochure LTV Nov 30 1956 34 Report No. R-219 Development of the US Army VZ 2

(Boeing Vertol -76) Research Aircraft Contract# Nonr 2136(00)

Aug 1963

141

35 Report No. 546.1 Proposal for the Design and Development of a Propelloplane Rescue Aircraft Hiller

Undated

36 Propelloplane Transport Study Summary Report Contract# Nonr 1637(00) Hiller

May 15 1956

37 Hiller VTOL/STOL Logistic Transport tilt Wing Propelloplane

Feb 1960

38 Miscellaneous Illustrations Tilt-Prop Aircraft Various

39 Tilt-Wing Applications by Blaine R. Parkin General Dynamics-Convair & Saul Bernstein Canadair

Sep 13-25 1969

TRI SERVICE TRANSPORT 72 1 Report No. 8069 VTOL Tri-Service Transport Model 175

– Summary McDonnell/Canadair Apr 3 1961

2 Report No. 8070 VTOL Tri-Service Transport Model 175 – Weight and Balance McDonnell/Canadair

Apr 3 1961

3 Report No. 8075 VTOL Tri-Service Transport Model 175 – Power Plant Installation and Fuel System McDonnell/Canadair

Apr 3 1961

4 Report No. 8076 VTOL Tri-Service Transport Model 175 – Hydraulic and Pneumatic Systems McDonnell/Canadair

Apr 3 1961

5 Report No. 8080 VTOL Tri-Service Transport Model 175 – Demonstration Program McDonnell/Canadair

Apr 3 1961

6 Report No. 8082 VTOL Tri-Service Transport Model 175 – Detail Specification McDonnell/Canadair

Apr 3 1961

7 Report No. 8083 VTOL Tri-Service Transport Model 175 – Contract Data Requirements McDonnell/Canadair

Apr 3 1961

8 Hiller Helicopter Model 1069 Rotor-Prop Convertiplane Undated 9 Briefing on the X-18 Research Aircraft and Future

V/STOL Aircraft Design Hiller Nov 11-13 1959

10 Memorandum Report on Safety Inspection – X-18 Tilt Wing VTOL Test Bed Contract# AF33(600)-32749 Hiller

Oct 27-28 1959

11 Report No. 101X90-2 The Kellett Direct Take-Off Airplane

Sep 1 1955 revA Sep 16 1955 revB Oct 4 1955

12 Report No. 106X90-3 Design Study Convertiplane Rotor System Contract# DA 44-177-TC-368 Kellett

Jan 1957

13 Report No. 106X90-1 The Kellett K-25 Flying Test Bed Feb 17 1956 revA Feb 24 1956 revB Feb 28 1956

14 Report No. G-113-36 The Model K-16B V/STOL Research Amphibious Aircraft: Summary Report

Mar 1967

142

Contract# NOa(s) 56-549c Kaman 15 Kaman K-16B Amphibian VTOL Presentation Undated 16 Report No. G-113-7 Estimated Flying Qualities of the

Kaman K-16B VTOL/STOL Aircraft Part II Dynamic Stability in Transitional Flight

Nov 20 1959

17 WADC TR 58-54 A Study of the Feasibility of Using a Semi-Rigid or Articulated Rotor System on a Tilt-Wing VTOL Airplane Part II Kaman

Apr 1958

18 Report No. R-219 Development of the US Army VZ-2 (Boeing-Vertol-76) Research Aircraft

Aug 1963

19 Boeing-Vertol Tilt Wing Development Program Undated

20 Report No. PR-378-20 Boeing-Vertol Model-137 Wind Tunnel Tests

May 22 1961

21 VHR-447 VTOL Tri-Service Transport Vol. 7 Summary report Part 1 Design Philosophy Hiller/Vought/Ryan

Undated

22 AFFTC Presentation – Introduction and Opening Remarks Oct 1966 23 History of the XC-142A Tri-Service Program 1967 24 XC-142A Lessons Learned Presentation Feb 5 1968 25 Report No. PDR-242-1 Part I Tri-Service VTOL Transport

Grumman Design 242 Proposal Summary Apr 3 1961

26 Report No. RAG-084-107 A Comparison of Downwash and Outflow from a Tilt-Wing Aircraft and a Helicopter Canadair

Feb 1971

27 Propeller Lifted Tilt-Wing VTOL Aircraft by Joseph Stuart III Hiller

Jan 23 1956

28 AIAA Paper No. 64-775 Survey of Significant Technical Problems Unique to V/STOL Encountered in the Development of the XC-142A by Lyman C. Josephs LTV

Sep 21-23 1964

29 XC-142A Brochure Undated 30 Report No. PDR-242-21 Grumman Design 242 Brochure Apr 17 1961 31 Ryan Reporter Vol. 22, No. 3 Tilt-Wing VTOL Nov 1961 32 NASA TN D-44 Force-Test Investigation of the Stability

and Control Characteristics of a 1/8-Scale Model of a Tilt-Wing Vertical-Take-Off-And-Landing Airplane

Aug 1959

33 NASA TN D-45 Flight Investigation of the Stability and Control Characteristics of a 1/8-Scale Model of a Tilt-Wing Vertical-Take-Off-And-Landing Airplane

Mar 1960

34 NASA TN D-390 Aerodymanic Characteristics of a ¼­Scale Model of a Tilt-Wing VTOL Aircraft at High Angles of Wing Incidence

Sep 1960

TRI-SERVICE TRANSPORT & TILT ROTOR 73 1 VTOL-STOL Progress Report Canadair Jan 1961

2 Report No. 299-099-128 Technical Considerations for Low-Disc-Loading V/STOL Aircraft of the Fixed-Wing

Dec 23 1959

143

and Tilt-Wing Configurations Bell 3 Report No. AER-E1R-13341 VHR-447 Volume 3 –

Performance Data Report Hiller/Vought/Ryan Undated

4 Report No. AER-E1R-13355 VHR-447 Volume 14 – SAC Charts Hiller/Vought/Ryan

Undated

5 Report No. ES 40302 Tri-Service Transport – Book 2 Summary Report (Technical) Douglas

Mar 31 1961

6 Report No. ES 40308 Tri-Service Transport – Book 8 Stability and Control Douglas

Mar 31 1961

7 Report No. ES 40385 Tri-Service Transport – Increased Primary Mission Capability – Model D-828A and D-829B Douglas

Jun 8 1961

8 Report No. ES 40459 Tri-Service Transport – Configuration Comparison – Canard Turboprop vs. Tilt Wing Douglas

Aug 3 1961

9 Report No. NA61H-497 Tri-Service VTOL Transport Supplemental Technical Data and Design Analysis North American

Aug 21 1961

10 Report No. PDR-242-5 Design 242 Stability and Control Part I Grumman

Apr 3 1961

11 Report No. PDR-242-5 Design 242 Stability and Control Part 2 Grumman

Apr 3 1961

12 Report No. PDR-242-6 Design 242 Wind Tunnel Test Part 2 Grumman

Apr 3 1961

13 Report No. PDR-242-6 Design 242 Wind Tunnel Test Part 3 Grumman

Apr 3 1961

14 Report No. PDR-242-6 Design 242 Wind Tunnel Test Part 4 Grumman

Apr 3 1961

15 Boeing-Vertol Model-137 Outline of Oral Presentation Apr 6 1961 16 Report No. PR-378-2 Model-137 Detail Specification

Boeing-Vertol Apr 1961

17 Report No. PR-378-3 Model-137 Weight and Balance Boeing-Vertol

Apr 1961

18 Report No. PR-378-5 Model-137 Stability and Control Boeing-Vertol

Apr 1961

19 Report No. PR-378-9 Model-137 Power Plant Installations and Fuel System Boeing-Vertol

Apr 1961

20 Report No. PR-378-10 Model-137 Hydraulic and Pneumatic System Boeing-Vertol

Apr 1961

21 Report No. PR-378-11 Model-137 Electrical System Boeing-Vertol

Apr 1961

22 Report No. PR-378-12 Model-137 Structural Description and Design Data Boeing-Vertol

Apr 1961

23 Report No. PR-378-13 Model-137 Structural Tests Boeing-Vertol

Apr 1961

24 Report No. PR-378-14 Model-137 Effects of Dimensional Apr 1961

144

Limitations Boeing-Vertol 25 Report No. PR-378-15 Model-137 Demonstration Program

Boeing-Vertol Apr 1961

26 Report No. PR-378-16 Model-137 Maintenance and Support Boeing-Vertol

Apr 1961

27 Report No. PR-378-19 Model-137 Alternate Rigid Propeller Boeing-Vertol

Apr 1961

SERIES VIII: Vertical Lift Theory and Aerodynamics – Non-Helicopter, 1932-1989

Box File Description Date

TRI-SERVICE TRANSPORTS HARRIER 74 1 Conversion of the Vought-Hiller-Ryan Tilt-Wing Tri-

Service Transport into the Fowler System of Deflected Slipstream VTOL by Harlan D. Fowler

May 23 1962

2 Application of the Fowler Principle of VTOL to the Wind Tunnel Model of Vought Tilt-Rotor V-447 by Harlan D. Fowler

Jul 20 1962

3 V/STOL Commercial Transport 18 Passengers or 5000lbs. Cargo Model 70 by Harlan D. Fowler

Nov 1964

4 NASA TN D-444 Lateral Stability and Control Characteristics of a Four-Propeller Deflected-Slipstream VTOL Model Including the Effects of Ground Proximity

Jan 1961

5 V/STOL Research Program for Low Cost Tactical Aircraft Feb 26 1970 6 V/STOL Research Program for Low Cost Tactical Aircraft

(Second Edition) Apr 10 1970

7 NASA TN D-444 Lateral Stability and Control Characteristics of a Four-Propeller Deflected-Slipstream VTOL Model Including the Effects of Ground Proximity

Jan 1961

8 TS 3056 Thrust Vectoring in Combat Rolls-Royce Oct 1978 9 V/STOL and the CV US Naval Institute Proceedings

October 1970 Article Oct 1977

10 The Jet V/STOL Harrier British Aerospace Jul 1978 11 FTD-HC-23-0664-72 The Harrier Avionics System Jun 23 1972 12 Chartered Mechanical Engineer Article Ski-Jump Jet Sep 1978 13 The British Aerospace Harrier, Case Study in Aircraft

Design Jul 1978

14 TS 3080 Vectored Thrust Jet V/STOL Dec 1978 15 XV-6A Carrier Suitability Testing US Naval Institute

Proceedings April 1967 + Harrier Handout Apr 1967

16 Testing the Kestrel by I. A. Fisher Sep 1965

145

17 Kestrel/Harrier Sketches 1956 18 Report 68-978-002 Stability and Control of the X-14

VTOL Research Airplane Contract#AF33(600)-30837 Bell Sep 5 1958

19 V/STOL Articles and Pictures Aviation Week 1977 20 Report 68-981-002 X-14 VTOL Research Progress Report

2 Contract# AF33(600)-30837 Bell Sep-Oct 1955

21 Report 68-981-007 X-14 VTOL Research Progress Report 7 Contract# AF33(600)-30837 Bell

Jul-Aug 1956

22 X-14 Articles and Pictures 1957

23 Report DCR-219 An Investigation of the Thrust Augmentation Characteristics of Jet Ejectors Contract# DA44-177-322(T) Dynasciences

c.a. 1967

24 WSWD-211 RV-X Air Sea Rescue and Recovery Design Study SOR 187 Northrop

Mar 7 1962

25 WSWD-209 RVX System Cost Analysis Northrop Jan 25 1962 26 NOR-62-113 Analytical Study of the VTOL Suckdown

Phenomenon Northrop Jul 31 1962

27 NOR-60-269 Research Study of a NORAIR Proposed VTOL Cascade Nozzle Northrop

Aug 1960

28 NOR-62-23 A Preliminary Human Engineering Control-Display Analysis for a VTOL Weapons System Northrop

Jan 29 1962

29 D3-3900-1 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing

Apr 3 1961

30 D3-3900-2 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing

Apr 3 1961

31 D3-3900-3 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing

Apr 3 1961

32 D3-3900-4 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing

Apr 3 1961

33 D3-3900-5 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing

Apr 3 1961

34 D3-3900-6 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing

Apr 3 1961

35 D3-3900-7 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing

Apr 3 1961

36 D3-3900-8 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing

Apr 3 1961

37 D3-3900-9 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing

Apr 3 1961

38 D3-3900-10 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing

Apr 3 1961

39 D3-3900-11 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing

Apr 3 1961

40 D3-3900-12 Proposal for a Tri-Service VTOL Prototype Apr 3 1961

146

Transport Aircraft Boeing 41 D3-3900-13 Proposal for a Tri-Service VTOL Prototype

Transport Aircraft Boeing Apr 3 1961

42 D3-3900-14 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing

Apr 3 1961

53 D3-3900-14 Proposal for a Tri-Service VTOL Prototype Transport Aircraft Boeing

Apr 3 1961

44 D3-3900 Loose Drawings Boeing Apr 3 1961

V/STOL 75 1 NASA SP-406 Powered Lift Aerodynamics and Acoustics May 24-26 1976

2 TM 761-98 Summary of the Development Work on Combination Helicopter and Fixed Wing Aircraft (Convertiplane or Heliplane)

Apr 14 1948

3 Jet Propulsion for Convertiplanes 1952 4 The Economies of VTOL Systems Apr 29 1966 5 Flight in the Earth’s Atmosphere, 1975-1985 May 17 1966 6 Report DAC 56017 Vertical Takeoff and Landing

Transports Douglas Jun 7 1966

7 VTOL Transportation Group Jun 28 1966 8 NACA TN3629 Investigation of the Effects of Ground

Proximity and Propeller Position on the Effectiveness of a Wing with Large Chord Slotted Flaps on Redirecting Propeller Slipstream Downward for Vertical Takeoff

Mar 1956

9 US/UK Advanced Short Takeoff and Vertical Landing (ASTOVL) Program + Pictures & Articles

Jul 31-Aug 2 1989

10 ETP 167 C/66616VTOL Surveillance System for the US Army Volume 1 Lockheed/Bendix

Aug 17 1959

11 ETP 167 C/66616VTOL Surveillance System for the US Army Volume 2 Lockheed/Bendix

Aug 17 1959

12 AFWAL-TR-82-3059 Proceedings: Ejector Workshop for Aerospace Applications

Jun 1962

13 Ejector Workshop for Aerospace Applications Aug 2-5 1981 14 A Jet Flap Diffuser Injector Oct 12 1971 15 NB66-204 VTOL Fighter System Trends Northrop May 1966 16 RAC 1012 Variable Sweep Wing Plus V/STOL Part 1

Aerodynamic Design Aspects Republic Dec 12 1962

17 RAC 1012-1 Variable Sweep Wing Plus V/STOL Part 2 Takeoff and Landing Performance Republic

Dec 12 1962

18 64-543Z V/STOL Design Studies c.a. 1964 19 NA-56-1418 Dispersed Site Fighter Bomber Briefing

Charts Undated

20 Report 44238 VTOL Advanced Tactical Fighter Configuration and Propulsion Study

Apr 25 1963

21 Dornier VTOL Pictures 22 Lift Jet Installational Experience Nov 14-18 1965

147

23 US Army VZ-11 Liftfan V/STOL Aircraft Pamphlet Undated 24 XV-5A Lift Fan V/STOL Aircraft Flight Test

Accomplishments c.a.1966

25 V/STOL Pictures and Articles 1962-1963 26 Dornier-Post V/STOL (in German) 1969

Location 52, File 3 V/STOL Aircraft Summary Chart Undated

VERTICAL TAKEOFF 76 1 AD 34451 Report CVAL 132A Additional Low-Speed

Wind Tunnel Tests on a 1/7 Scale Model of the Ryan Model R-38 Helicopter: Volume I & II, Force Data: Investigation of Various Vertical Tails, Modified Wing Tips and Roll Jets Ryan

Dec 16 1953

2 NASA TN D-404 Hovering and Transitional Flight of a 1/5 Scale Model of a Jet Powered Vertical Altitude VTOL Research Aircraft Ryan

May 1961

3 Report 6954-7 General Flying Qualities in the Conventional Flight Regime Based on Flight Test Results: USAF Model X-13 Airplane Contract# AF33(600)-25895 Ryan

May 11 1956

4 Report 6955-1 Systems Analysis Report on USAF Model X-13 Airplane Stabilization System Contract# AF33(600)­25895

Mar 15 1956

5 Report 6927-12 Performance Report; Rolls-Royce RA-28­49 Turbojet as Installed in the X-13 Research Aircraft Contract# AF33(600)-25895

Aug 1 1954

6 Report 6910-25 Project MX-1976 Monthly Progress Report- X-13 – Vertical Takeoff Research Airplane (Ryan Model 69) Contract# AF33(600)-25895

Sep 1 1955

7 Report 6910-7 Estimated Aerodynamic Performance of USAF X-13 Airplane Contract# AF339600)-25895

1 August 1954

8 Tail Sitting Fighters, Article and Photos(X-13) Undated 9 D189-14797-1 Sea Control Fighter System Development

Proposal Boeing Jan 10 72

10 Convair XFY-1 “POGO” Photograph Undated 11 Proposal G.O. 20438 for Construction of Heliplane; Model

XGEH-1C General Electric Feb 8 1944

12 LR 26175 Final Report VTOL Strike RPV Study Contract# F33657-74-C0190 Lockheed

Dec 12 1973

13 Report CVAL 132B Additional Low-Speed Wind-Tunnel Tests on a 1/7 Scale Model of the Ryan Model R-38 To Investigate a Modified Vertical Tail and an Elevon to

Mar 12 1954

148

Increase Span 14 N79-10026 Study of Aerodynamic Technology for VSTOL

Fighter/Attack Aircraft – Vertical Attitude Concept May 1978

15 Wind Tunnel Photos of FW 860 Jet Fighter c.a. 1960 16 Photo Negatives of FW -860 Aircraft c.a. 1960 17 Photo Prints of FW-860 Aircraft 1960 18 Propeller Driven Vertical Altitude Takeoff and Landing

Concepts for Remotely Piloted Vehicles Dec 21 1976

19 Grumman Aerospace Horizons, Vol.12 no.3 Revolutionary V/STOL for Small Ships Magazine

1976

20 Bell Aerospace LFV and MFS Pamphlets 1964-1965 21 NASA Memo 5-7-59L Flight Investigation of Effects of

Transition, Landing Approaches, Partial-Power Vertical Descents and Droop-Stop Pounding on the Bending and Torsional Moments Encountered by a Helicopter Rotor Blade.

May 1959

22 NASA TN D-818 Method for Calculating Induced Velocities at the Blades of a Slightly Inclined Propeller with Constant Circulation

May 1961

23 NASA TN D-404 Hovering and Transition Flight of a 1/5 Scale Model of a Jet Powered Vertical-Altitude VTOL Research Aircraft

May 1961

24 Ryan Model 115C Vertical takeoff Aircraft Proposal Dec 3 1957 25 SNECMA Pamphlet for C400 P-2 ATAR Volant (in

French) May 14 1957

26 SNECMA Pamphlet for C.450 “Coleoptere ( in French) Jun 1967 27 “Nutcracker VTOL System Concept and Articles

Grumman 1976

28 XFV-1 VTOL Fighter, Articles and Pictures undated 29 Propeller Driven Vertical Altitude Takeoff and Landing

Concepts for Remotely Piloted Vehicles Dec 21 1976

30 NACA RM L51H13a Dynamic Stability and Control Characteristics of a Delta-Wing Vertically Rising Airplane Model in Takeoffs, Landings and Hovering Flight

Oct 9, 1951

31 NACA RM53G27 Wind-Tunnel Investigation at Low Speed of the Pitching Stability Derivatives of a 1/9 Scale Powered Model of the Convair XFY-1 Vertically Rising Aircraft

Jul 23 1953

32 NACA RM SL54B03a Flight Determination of the Longitudinal Stability Characteristics of a 0.133 Scale Rocket Powered Model of the Consolidated Vultee XFY-1 Airplane Without Propellers at Mach Numbers from 0.73 to 1.19

Feb 14 1954

33 NACA RM SL53E13 Wind-Tunnel Investigation at Low Speed of the Rolling Stability Derivatives of a 1/9 Scale Powered Model of the Convair XFY-1 Vertical Rising

May 20 1953

149

Aircraft 34 NACA RM SL53B20 Wind-Tunnel Investigation at Low

Speed of the Static Longitudinal and Lateral Stability Characteristics of a 1/9 Scale Powered Model of the Convair XFY-1 Vertically Rising Aircraft

Feb 11 1953

35 NACA RM SL52L10 Investigation of Spinning and Tumbling Characteristics of a 1/20 Scale Model of the Consolidated Vultee XFY-1 Airplane in a Free Spinning Tunnel

Dec 10 1952

36 NACA RM SL54F11 Longitudinal Stability Characteristics of the Consolidated Vultee XFY-1 Airplane with Windmilling Propellers as Obtained from Flight of 0.113 Scale Rocket Propelled Model at Mach Numbers from 0.70 to 1.13

Jun 11 1954

37 NACA RM SL52I26 Stability and Control Flight Tests of a 0.13 Scale Model of the Consolidated Vultee XFY-1 Airplane in Takeoffs, Landings and Hovering Flight

Oct 1 1952

38 NACA RM SL53E18 Flight Investigation of the Stability and Control Characteristics of a 0.13 Scale Model of the Convair XFY-1 Vertically Rising Aircraft During Constant Altitude Transitions

May 21 1953

39 NACA RM SL54E07 Flight Tests of a 0.13 Scale Model of the Convair XFY-1 Vertically Rising Airplane with the Lower Vertical Tail Removed

May 12 1954

40 NACA RM SL54C19a Vertical Descent and Landing Tests of a 0.13 Scale Model of the Convair XFY-1 Vertically Rising Airplane in Still Air ( 2 copies)

Mar 16 1954

41 NACA RM SL53D01 Wind-Tunnel Investigation at Low Speed of the Yawing Stability Derivatives of a 1/9 Scale Powered Model of the Convair XFY-1 Vertically Rising Aircraft

Mar 31 1953

42 NACA RM SL54E28 Takeoff and Landing Characteristics of a 0.13 Scale Model of the Convair XFY-1 Vertically Rising Airplane in Steady Winds

Jun 23 1954

43 NACA RM SL54B16a Flight Tests of a 0.13 Scale model of the Convair XFY-1 Vertically Rising Airplane in a Setup Simulating That Proposed for Captive Flight Tests in a Hanger

Feb 12 1954

44 P.F.Girard (Test Pilot) 2 Articles on Vertical Attitude Jet Powered Airplanes

1953

45 Report 239 Medical and Human Engineering Aspects of Flight In Ryan VTOL and STOL Aircraft

May 1959

46 NACA RM SL53E18 Flight Investigation of the Stability and Control Characteristics of a 0.13 Scale Model of the

May 21 1953

150

Convair XFY-1 Vertically Rising Aircraft During Constant Altitude Transitions

47 NACA RM L56H29a Dynamic Model Investigation of Two Tail-Sitter Vertically Rising Airplanes to Determine the Altitude Required to Approach Normal-Flight Conditions After Power Failure on Hovering Flight

Nov 9 1956

48 NACA RM SL53B20 Wind-Tunnel Investigation at Low Speed of the Static Longitudinal and Lateral Stability Characteristics of a 1/9 Scale Powered Model of the Convair XFY-1 Vertically Rising Aircraft

Feb 11 1953

49 NACA RM SL53E13 Wind-Tunnel Investigation at Low Speed of the Rolling Stability Derivatives of a 1/9 Scale Powered Model of the Convair XFY-1 Vertical Rising Aircraft

May 20 1953

50 Rolled Diagrams of Northrop VATOL Aircraft Apr 18 1978

V/STOL PROPELLER TECHNOLOGY CONCEPTS 77 1 Report No. LB-30684 Advanced STOL Assault &

Logistics Transport Model 2217 Douglas Aircraft Oct 12 1961

2 Report No. LB-30652 Advanced STOL Assault & Logistics Transport Model 2217A Douglas Aircraft

Apr 12 1962

3 Report 30959 STOL Turboprop Assault Transport Model 2252 Douglas Aircraft

Jul 20 1962

4 AIAA Paper No. 71-982 Canada’s STOL Program – A Progress Report by C.C. Halton Ministry of Transport (Canada)

Oct 25-28 1971

5 AIAA Paper No. 71-983 The Trends of the STOL System by M. Avramito Aerospatiale

Oct 25-28 1971

6 AIAA Paper No. 71-990 Performance Prediction and Evaluation of Propulsion-Augmented High Lift Systems by R.L. Gielow Lockheed Georgia

Oct 25-28 1971

7 STOL Aircraft Technology in Relation to Military/Civilian Requirements by Marvin D. Marks & James P. Caldwell McDonnell Douglas

Sep 23 1969

8 AIAA Paper No. 71-578 Douglas Paper 5928 Recent Developments in Jet Flap Theory and its Application to STOL Aerodynamic Analysis by M.L. Lopez & C.C. Shen McDonnell Douglas

Jun 21-23 1971 rev. Jul 23 1971

9 Report LR 23916 60-Passenger STOL Test Aircraft for NASA Flight Research Center Lockheed-California

Sep 2 1970

10 Report MDC 69-027 (Paper C-WP 2.1) Simulation of STOLport Runway and Gate Operations by J.E. Hosford & J.R. Lovit McDonnell Douglas

Nov 10-12 1969

11 Report AERO.2645 Theoretical Analysis of a Gust Alleviator Used on a Lancaster Aircraft and Comparison

Jan 1961

151

with Experiment by J.K. Zbrozek British Ministry of Aviation

12 Report MCL-927/1+2 The STOL Dornier Jun 26 1961 13 AEREON Dynairship – History and Articles 1973 14 NASA SP-320 STOL Technology Oct 17-19 1972 15 USAAMRDL TR 73-34A Summary of Propeller Design

Procedures and Data Volume I – Aerodynamic Design and Installation

Nov 1973

16 USAAMRDL TR 73-34A Summary of Propeller Design Procedures and Data Volume II – Structural Analysis and Blade Design

Nov 1973

17 USAAMRDL TR 73-34A Summary of Propeller Design Procedures and Data Volume III – Hub, Actuator and Control Designs

Nov 1973

18 NACA ARR No. 3E19 Formulas for Propellers in Yaw and Charts of the Side-Force Derivative

May 1943

19 NACA ACR No. L4I19 The Theory of Propellers II – Method for Calculating the Axial Interference Velocity

Nov 1944

20 NACA ACR No. L4J10 The Theory of Propellers III – The Slipstream Contraction with Numerical Values for Two-Blade and Four-Blade Propellers

Nov 1944

21 NACA ARR No. 3L09 Propellers in Yaw Dec 1943 22 NACA RB No. 3L02 Proposal for a Propeller Side Force

Factor Dec 1943

23 NACA ACR No. L5F30 Effect of the Lift Coefficient on Propeller Flutter

Jul 1945

24 NASA TN D-434 Low-Speed Investigation of a Full-Span Internal-Flow Jet-Augmented Flap on a High-Wing Model with a 350 Swept Wing Aspect Ratio 7.0

Aug 1960

25 AEDC-TR-72-139 Simulation of a High Disc Loading Free Propeller in a Cross Flow by the Vortex-Lattice Method

Nov 1972

26 WADC TR 58-564 Study of Propeller Controls for VTOL Aircraft Applications

Dec 31 1958

27 Q-FAN Generalized Performance, Noise and Weight Data for Sev Applications

Jan 25 1972 rev Jul 15 1972

28 NASA CR111842 Prop-Fan Results of Initial Prop-Fan Model Acoustic Testing Volume I – Discussion

Dec 4 1970

29 NASA CR111842 Prop-Fan Results of Initial Prop-Fan Model Acoustic Testing Volume II Appendices B thru F

Dec 4 1970

30 NASA CR111956 Results of Prop-Fan/STOL Wing Acoustics Tests

Jul 29 1971

31 Hamilton Standard Letter to Aeronautical Engine Laboratory , Naval Air Engineering Center

Sep 9 1966

32 USAAVLABS TR 68-33 Extracts Feasibility Study for Advanced V/STOL Propeller Technology

Undated

152

33 Report No. 8820-2 Propeller Static Thrust Ryan Aeronautical Co.

Aug 24 1955

34 Propeller and Gearbox Propulsion Technology Forecast (Rough Draft)

1985

35 DOWTY Variable Pitch Fans with Cover Letter Nov 12 1971 36 Q-FAN Performance and Scaling Data for Two Q-FAN

Design Undated

37 Prop-Fan Generalized Performance Hamilton Standard May 18 1970 rev1 Aug 28 1970 rev2 Jun 1973

38 Physics and Flow of a Propeller and Rotor System by Paul E. Williams MDC

1970

39 Physics and Flow of a Propeller and Rotor System Supplement 1 by Paul E. Williams MDC

May 11 1970

LIFT-FAN 78 1 Lift Fan Flight Research Aircraft Program Quarterly

Technical Progress Report No 1 Contract# DA44-177-TC­715 GE

Mar 31 1962

2 Lift Fan Flight Research Aircraft Program Quarterly Technical Progress Report No 2 Contract# DA44-177-TC­715 GE

Jun 30 1962

3 Lift Fan Flight Research Aircraft Program Quarterly Technical Progress Report No 3 Contract# DA44-177-TC­715 GE

Sep 30 1962

4 Lift Fan Flight Research Aircraft Program Quarterly Technical Progress Report No 4 Contract# DA44-177-TC­715 GE

Dec 31 1962

5 Lift Fan Flight Research Aircraft Program X353-5B Propulsion System Flightworthiness Test Report Volume 1 Contract# DA44-177-TC-715 GE

Jan 1963

6 Lift Fan Flight Research Aircraft Program Quarterly Technical Progress Report No 5 Contract# DA44-177-TC­715 GE

Apr 30 1963

7 Lift Fan Flight Research Aircraft Program Quarterly Technical Progress Report No 6 Contract# DA44-177-TC­715 GE

Jun 30 1963

8 Lift Fan Flight Research Aircraft Program Quarterly Technical Progress Report No 7 Contract# DA44-177-TC­715 GE

Sep 30 1963

9 Lift Fan Flight Research Aircraft Program Quarterly Technical Progress Report No 8 Contract# DA44-177-TC­715 GE

Dec 31 1963

10 Lift Fan Flight Research Aircraft Program Quarterly Technical Progress Report No 10 Contract# DA44-177­

Jul 1964

153

TC-715 GE 11 Lift Fan Flight Research Aircraft Program Quarterly

Technical Progress Report No 11 Contract# DA44-177­TC-715 GE

Oct 1964

12 Report NB-61-140 Northrop N-267 Fan-In-Wing Flight Research Aircraft Program Volume I – Description of Technical Program

May 1961

13 Report NB-61-140 Northrop N-267 Fan-In-Wing Flight Research Aircraft Program Volume III – Aircraft Specification NS-145 (Preliminary)

May 1961

14 Report NB-61-140 Northrop N-267 Fan-In-Wing Flight Research Aircraft Program Powered Model Tests and Data Analysis

Jun 1961

15 Report NB-61-140 Northrop N-267 Fan-In-Wing Flight Research Aircraft Program Refinement and Substantiation of Technical Proposal

Jul 1961

16 An Analysis of a Two-Dimensional Propulsion Wing by Galen Hu Stanford University

1971

17 XV-5A Contractor Flight Test and Evaluation 1964-1965 18 Report No. 62B133 Operational V/STOL Ryan Jan 1 1963 19 Report AD 657 992 X353-5B Propulsion System

Flightworthiness Test Report Volume 1 Contract#DA44­177-TC-715 GE

Jan 1963

20 DADD TR 60-371 Volume II Study of Submerged Fan Type VTOL Aircraft Contract#AF33(616)-6605 GE

Mar 1960

21 NASA CR-761 Lift Fan Technology Studies Contract# NAS 2-3077

Apr 1967

22 Vanguard Model 3 VTOL/STOL Rescue Aircraft -Aircraft Characteristics

Undated

23 Appraisal of Comparative Evaluation Fan-In-Wing versus Adam II LTV Vought

Jan 10 1964

24 Lift Fan Thrust Augmentation Aircraft – Illustrations, Articles and Photos

1964-1965

25 Report PR-316 Proposal for a Wind Tunnel Program to Study “Jet Wall” Applications to Wing-Submerged Ducted Fans Vertol

Jun 17 1959

26 NASA TN D-731 Induced Interference Effects on Jet and Buried-Fan VTOL Configurations in Transition

Mar 1961

27 Report 25-X-2 Vanguard Heavy Lift System for Transportation of Very Large Military Equipment

Jan 15 1962

28 Feasibility Study of a M3 Fighter Airplane with Lift Fans for V/STOL Operations Ryan

Jan 17 1963

29 Report No. 62B136 Planning Proposal for XV-5A V/STOL Operational Evaluation Aircraft – Ryan Model 167

Dec 12 1962

154

30 Report No. 63B045 V/STOL Weapon System Development Plan Ryan & Raytheon

May 10 1963

31 Report No. 290-70-2 Proposal for F-104 Fan Design Study – Ryan Model 190D

May 28 1965

STRUCTURES/AERODYNAMICS 79 1 Report #25 Flight Research Investigation of Laminar

Separation of a High Lift Boundary Layer Control Airplane by Dezso Gyorgyfalvy Mississippi State Univ.

Jun 26 1959

2 Model 34 Aerodynamic Report 158 Analysis of Model 34 Wind Tunnel Tests Beech

Dec 27 1945

3 Model 38 Aerodynamic Report 238 Analysis of Model 38 Wind Tunnel Tests Beech

Jun 3 1947

4 Model 305 Report No. 951 Flight Test Performance Cessna

Mar 17 1950

5 Report F-TS-668-RE The Influence of Fuselage and Wing Sweepback on the Range and Speed of Turbo-Jet Airplanes by Siegfried Gunter (Heinkel) (Germany)

Sep 1946

6 Airpower Journal Air Occupation –Asking the Right Questions by MAJ Marc K. Dippold USAF

1997

7 NASA CR-137894 Civil Uses of Remotely Piloted Vehicles (Final Report) Contract# NAS 2-8935

Jul 1976

8 NASA CR-137895 Civil Uses of Remotely Piloted Vehicles (Summary Report) Contract# NAS 2-8935

Jul 1976

9 Paraglider Recovery Systems by Francis M. Rogallo NASA

Apr 30-May 2 1962

10 NASA Research on Flexible Wings by Francis M. Rogallo NASA

Apr 3-6 1967

11 Parawings for Astronautics by Francis M. Rogallo NASA Sep 10-12 1963 12 An Aviation Milestone – Man Achieves the Age Old Goal

of Self-Powered Flight by Peter B.S. Lissaman The Gossamer Condor

1977

13 Report No. 5069 Performance Flight Testing Methods in Use by the Flight Section AAF Technical Service Command, Wright Field

Jan 15 1944

14 AAF Inspector’s Familiarization Manual – Midwest Procurement District, Material Command

Mar 1 1943

15 AAF TR 5242 Stability and Control Flight Test Methods Jul 14 1945 16 Report ANC-18 Design of Wood Aircraft Structures Jun 1944 17 Report ANC-19 Wood Aircraft Inspection and Fabrication Dec 20 1943 18 DR Report No. 1139 Aircraft Design Analysis Methods as

Employed by The Research Division of BuAer Oct 6 1949

19 Report TN-70-AM-01 Drag Estimation Procedures for Preliminary Design Configuration Studies General Dynamics

Mar 23 1970

20 ANA Bulletin No. 421 Atmospheric Properties – Extreme Sep 24 1953

155

Cold and Hot; Standard for Aeronautical Design 21 ANC-5 Strength of Metal Aircraft Elements Mar 1955 22 ANC-5a Strength of Metal Aircraft Elements Rev May 1949 23 AAF TR 5193 A Method for Estimating Gas Turbine – Jet

Airplane Performance Mar 8 1945

24 Simplified Methods of Horsepower Correction for Single-Speed and Two-Speed Engines Wright Aeronautical Corp.

Apr 1944

25 Engineering Notes Wright Aeronautical Corp. Undated 26 Homebuilt Airplanes – Articles Various 27 Bede 5 Aircraft Information Various

28 “Toward New Horizons” A Report to General of the Army H.H. Arnold by Thomas Von Karman

Nov 7 1944

29 FTD-TT-65-1573 Aircraft Construction (Selected Parts) (Russian)

Undated

30 Ocean Surveillance and Control Boeing Nov 1972 31 The Potential Contribution of Subsonic Aviation to Short

Haul Transportation by R.H. Miller MIT Apr 1967

32 FS-26 Concept (IN German) Undated 33 The De Havilland Dragon – Six Apr 26 1934 34 NACA Report L4D18 Stability of a Body Stabilized by

Fins and Suspended from an Airplane Apr 1944

35 NACA Memorandum Report of Oct 1942 A Flight Investigation of the Stability of a Towed Body

Oct 1942

36 NACA Report 3K17 Theoretical Analysis of the Lateral Stability of a Glider Towed by Twin Parallel Tow Lines

Nov 1943

37 Project 72011461 Advanced Systems Concepts Lockheed May 31 1972 38 Report TM 73-38 PTT Teleplane Progress Report Apr 1973 39 Report ST-CS-01-147-72 DIA Task T70-01-13

Aerodynamics (Research and Development) Free World Sep 21 1972

40 Unmanned Aerial Vehicle (UAV) Master Plan 1992 Apr 15 1992 41 Unmanned Aerial Vehicle (UAV) Master Plan 1993 Mar 31 1993 42 Aircraft Photos – Miscellaneous Most WW II Undated

VTOL 80 1 FSTC-HT-23-967-68 Vertical Landing and Takeoff

Aircraft (USSR) 1966

2 Symposium on Vertical and Short Take-Off and Landing Aircraft Part 2 (NATO)

Jun 1960

3 Report Beyond the Horizon Flight in the Atmosphere, 1975-1985 Volume III Vertical Takeoff and Landing

Jan 1967

4 Report D8-2194-1 Drag Estimation of V/STOL Aircraft Boeing

Sep 20 1968

5 Research and Development of Advanced Rotorcraft Concepts by Evan A. Fradenburgh Sikorsky

Feb 17-19 1969

6 Systems Considerations in VTOL Notes by C.C. Wood May 17 1966

156

Sikorsky 7 Foreign VTOL Progress Draft and Slides Undated 8 Contributions of Bell Helicopter Company to Helicopter

Development by Bartram Kelley Undated

9 US Navy VSTOL Technology Assessment Volume II Final Report

Jun 1975

10 Deployable Airfoil Structure and Application Parsons Corp.

Undated

11 Report PB 111633 Special Types of Rotary Wing Aircraft Volume II Contract# W33-038-ac-21804(20695)

1954

12 Joint DOD-NASA-DOT Study – R&D Contributions to Aviation Progress (RADCAP) Volume II Appendices 1 thru 9

Mar 1972

13 NASA V/STOL and STOL Conference – Program and Slides

Apr 4-5 1966

14 AHS 1st National V/STOL Aircraft Symposium Supplement

Nov 3-4 1965

15 Report 60WWR-930 SR-175 V/STOL Logistic Aircraft Study Vol. I Appendix Contractor Report Summaries

Jun 1960

V/STOL AERODYNAMICS 81 1 Ryan Reporter Vol.22 No.3; Vol.23 No.1; Vol 23 No.2 Nov 1961- Mar

1962 2 Project No. AU-419-63-ASI Test and Evaluation of

Combat Functions May 1963

3 AFFDL TM-73-4-PTC Assessment of VTOL Concepts for RPV Applications

Jan 17 1973

4 Report No. 5 Development of Methods for Predicting V/STOL Aircraft Characteristics Contract# Nonr 3099(00)

Apr 15 1960

5 AFFDL TM-73-100-PTB Design Investigation of Three Vertical Landing Concepts for RPV Application, Phase II

Aug 1973

6 Report PR-107 Proposal for the Advancement of Techniques for Very Large Vertical Lift Systems Vanguard Air and Marine Corp.

Jan 15 1962

7 Report PR-316 Proposal for a Wind Tunnel Program to Study “Jet Wall” Applications to Wing-Submerged Ducted Fans Vertol

Jun 17 1959

8 NASA TN D-4448 Large-Scale Wind-Tunnel Tests of a Deflected Slipstream STOL Model with Wings of Various Aspect Ratios

Mar 1968

9 Report TR-29 An Experimental Investigation of an External Aerodynamic Diffuser Contract# N00014-68-A­0512 West Virginia University

Apr 1971

10 Report 64-1 Hiller Model 1117 Light Armed Reconnaissance V/STOL Aircraft with Associated Documentation

Mar 1964

157

11 Report 64-1 Hiller Model 1117 Light Armed Reconnaissance V/STOL Aircraft Reference 2

March 1964

12 Air Products Co. Proposal VTO Lift & Transport Vehicle (Heavy Duty)

Undated

13 Air Products Co. Scientific & Technical Brochure Undated 14 Report APR-64-4 Investigation of the Process of Energy

Transfer from an Intermittent Jet to Secondary Fluid in an Ejector-Type Thrust Augmenter – Interim Summary Report Covering the Period Oct 30 1962 to Mar 31 1964 Contract# Nonr 3082(00)

Mar 31 1964

15 Report No. 298 Hiller Pulse Reactor Lift-Propulsion Engine

Feb 1962

16 Report ARL 71-0236 The Performance Characteristics of the 7/10’s Nozzles in the Five Foot Single Channel Vertical Ejector

Oct 1971

17 Report No. 2099-928003 A Generalized Experimental Study of Inlet Temperature Rise of Jet V/STOL Aircraft in Ground Effect Contract# BuWeps N600(19)63320

Apr 5 1966

18 NASA TN D-372 A Flight Study of the Conversion Maneuver of a Tilt-Duct VTOL Aircraft

Nov 1960

19 WADC TR 58-630 Study of Propeller Controls for VTOL Aircraft Applications (Item III-Final TR) Contract# AF 33(616)5294

Undated

20 Report PSAD-78-61 Status of the Navy’s Vertical Short takeoff and Landing Aircraft

Feb 23 1978

21 V/STOL Type A Technical Briefing Lockheed-California Jul 26 1977 22 Ryan Reporter 1964 23 Report LR 19755 Advanced Transport Aircraft 1975-1985

Lockheed-California May 19 1966

24 Report NA-70-327-1 VTOL Integrated Flight Control System R&D Final TR Volume I Technical Summary

1969

25 Report R60FPD148 SR-175 VTOL/STOL Logistics Aircraft Volume II – TR Parametric Study

Mar 1960

26 Report ASD-TDR-62-578 Suppression of Jet Noise with Emphasis on the Near Field

Feb 1973

27 Report EWR-Nr. 4-66 Experience with the Flight Test Instrumentation System of the VTOL Aircraft VJ 101 C.

Mar 21-24 1966

28 NAVAIR-1R-76 USN/FMOD FRG VAK-191B Joint Flight Test Program Final Report Volume No. 1 Summary

Aug 1976

29 V/STOL Handling Qualities Criteria Compared with Flight Test Results of the V/STOL – Supersonic Fighter VJ 101 C and the V/STOL – Transport Aircraft DO-31 E Dornier-MBB

Sep 28-Oct 1 1971

30 Alternate Designed/Propulsion Concepts for a Low-Signature, Small Military transport by Charles Patterson , Jon Champion & Lt. Ken Sebek Wright Labs, WPAFB

Undated

158

31 Using New Technology – The AV-8B Harrier II by Stan Lewis Rockwell

Undated

32 Report ER 4222 New Surveillance Aircraft System Parametric Study 1965-1970 Time Frame

Feb 1 1960

33 Report 64-1 Hiller Model 1117 Light Armed Reconnaissance V/STOL Aircraft Reference 3

Mar 1964

34 Report 14647 CL-519 Lockheed V/STOL Utility Aircraft Undated 35 Report 64-1 Hiller Model 1117 Light Armed

Reconnaissance V/STOL Aircraft Reference 1 Mar 1964

36 WRDC-TR-89-6011 Special Operations Forces (SOF) Transport Aircraft Study Volume I: Executive Summary

Jan 1990

37 WRDC-TR-89-6011 Special Operations Forces (SOF) Transport Aircraft Study Volume II: Technical Analysis

Jan 1990

38 WRDC-TR-89-6012 Special Operations Forces (SOF) Transport Aircraft Study Volume I: Executive Summary

Jan 1990

39 WRDC-TR-89-6012 Special Operations Forces (SOF) Transport Aircraft Study Volume II: Technical

Jan 1990

40 AIAA Papers No. 71-576: No. 74-995 1971/1974 41 SURVIAC-TR-91-008 Special Operations Aircraft

Technology Assessment – V/STOL Compendium and Database

Dec 1990

VTOL RESEARCH 82 1 Report No. G-113-1 Design Detail Specification for Model

K-16B Wind Tunnel Model Contract# NOa(s) 56-549c Kaman

Jun 30 1958

2 Report 9433 Proposal for Study of VTOL Day Fighter Lockheed

Oct 9 1953

3 Report No. G-113-3 Pilot Compartment Mock-Up review Kaman

Feb 12 1959

4 Report No. G-90 Experimental Investigation of a Trailing Edge Flap as a Means of Propulsive Rotor Cyclic Pitch Control of VTOL/STOL Aircraft Contract# NOA(S) 56­549C Kaman

Apr 27 1956

5 Report No. R-183A An Alternate Proposal for the Design, Construction and Test of the K-16B VTOL/STOL Research Aircraft Kaman

Jan 29 1958

6 Report No. G-111-1 An Experimental Investigation of a Cyclic Pitch Controlled Rotoprop for VTOL/STOL Aircraft Part 1 Design and Planning Contract NOa(s) 56­549c Kaman

Jun 15 1958

7 Report No. G-111-2 An Experimental Investigation of a Cyclic Pitch Controlled Rotoprop for VTOL/STOL Aircraft Part II Test Operation and Structural Evaluation

Nov 5 1958

8 Report No. G-111-3 An Experimental Investigation of a Aug 1958

159

Cyclic Pitch Controlled Rotoprop for VTOL/STOL Aircraft Part III Controllability Contract# NOa(s) 56-549c Kaman

9 Report No. G-111-4 An Experimental Investigation of a Cyclic Pitch Controlled Rotoprop for VTOL/STOL Aircraft Part IV Performance Contract# NOa(s) 56-549c Kaman

Sep 1958

10 Report No. G-113-2 Methods of Analysis for Free Flight Loading Conditions Contract# NOa(s) 56-549c Kaman

Dec 12 1958

11 Report No. G-113-4 Estimated Flying Qualities of the Kaman K-16B VTOL/STOL Aircraft Contract# NOa(s) 56-549c Kaman

Feb 20 1959

12 Report No. G-113-5 K-16B Calculated Airloads Report Contract# NOa(s) 56-549c Kaman

Jul 15 1959 Rev.A Jan 6 1960

13 Report No. G-113-6 Flutter Analysis of the Kaman K-16B VTOL/STOL Research Aircraft Contract# NOa(s) 56-549c Kaman

Oct 15 1959

14 Report No. G-113-8 Model K-16B Estimated Weight and Balance Contract# NOa(s) 56-549c Kaman

Dec 18 1959

15 Report No. G-113-10 Mechanical Instability Analysis of the Kaman K-16B VTOL/STOL research Aircraft Contract# NOa(s) 56-549c Kaman

Jan 15 1960

16 Brochure No. B-12 The Model K-16B Research Amphibian Contract# BUAER NOa(s) 56-549c Kaman

Oct 30 1959

17 Kaman K-16B Hover Undated 18 Report No. 10699 Flight Tests of the Lockheed XFV-1 Jun 15 1955 19 M=1.2 Fighter Attack Technology Lockheed May 31 1972 20 Report No. 9122 Aerodynamic Characteristics of the

Lockheed XFV-1 in the Hovering and Transition range Lockheed

Jun 1 1953

21 Turboprop Propulsion/Control System for Transonic V/STOL Military Aircraft Lockheed-California

Feb 15 1972

22 AERO Report 902 Wind-Tunnel Tests of a 1/16-Scale Model of a Rotatable-Wing Seaplane Part II – Longitudinal and Lateral Characteristics

Dec 1959

23 V/STOL Propulsive Rotor – Recommendations for Further Research Kaman

Dec 5 1968

24 Report LR 25170 Proposal for Turboprop Propulsion/Control System for Transonic V/STOL Aircraft Lockheed-California

Mar 1972

25 Report LR 24441-1 Research Program for M=1.2 V/STOL Tactical Fighter Lockheed-California

Apr 6 1971

26 Report No. 8072 VTOL Tri-Service Transport Model 175 Stability and Control McDonnell/Canadair

Apr 3 1961

160

27 FDV 9-7-13 VC-400 Cargo and Passenger Aircraft Undated 28 Non-Rotary Wing Aircraft research by John P. Rabbott, Jr.

Sikorsky Jul 11 1963

29 Report 224-41-61 Analysis of a Wind Tunnel Test of a 0.08 Scale Tilt-Wing VTOL Model, NACAL #59

Apr 28 1961

30 Report No. 8077 VTOL Tri-Service Transport Model 175 Structural Description and Design Data McDonnell/Canadair

Apr 3 1961

31 Tilt-Wing Photos Undated

HIGH LIFT DEVICES 83 1 Louis Breguet 1911-1961 Commemorative Booklet (in

French) May 15 1961

2 Breuget Aviation Facilities and Aircraft Brochure C.A. 1970 3 Reports and Memoranda No. 1520 Air Torque on a

Cylinder Rotating in an Air Stream by A. Thom & S.R. Sengupta U. of Glasgow

Oct 22 1932

4 Reports and Memoranda No. 1623 On the Effect of Discs on the Air Forces on a Rotating Cylinder by Alexander Thom U. of Glasgow

Jan 5 1934

5 USAAVLABS TR 66-39 Principles for Improving Structural Crash Worthiness for STOL and CTOL Aircraft

Jun 1966

6 Custer Channel Wing, Information Submitted to W.J. Boyne by B. Lindenbaum

Nov 30 1976

7 Custer Channel Wing – Assessment Jan 1971 8 Custer Channel Wing – Correspondence 1971 9 STOL – Miscellaneous Articles and Photos C.A. 1970 10 Hispano-Suiza Flexible Transmission System for Breguet

943 Aircraft Jul 17 1962

11 TR No. RCF-1 A Study of the Aerodynamic Characteristics of a High-Lift Device Based on a Rotating Cylinder and Flap Contract# NONR-225(54) (NR 212­217) Stanford Univ.

Sep 1961

12 ER No. 249 Evaluation of the Performance, Stability and Control of the Helio Coutier Airplane – Progress Report for Oct 1956 Contract# DA 44-177-TC-369 Univ. of Wichita

Nov 1956

13 ER No. 252 Evaluation of the Performance, Stability and Control of the Helio Coutier Airplane – Progress report for Nov 1956 Contract# DA 44-177-TC-369 Univ. of Wichita

Dec 1956

14 ER No. 260 Evaluation of the Performance, Stability and Control of the Helio Coutier Airplane – Progress report for Dec 1956 Contract# DA 44-177-TC-369 Univ. of Wichita

Jan 1957

15 Report No. 1 Lift Characteristics of Wings Extending Through Propeller Slipstreams Contract# Nonr 2388(00) VRC

Sep 1958

161

16 Report D210-10201-1 STOL High Lift Design Study Contract# USAF F33615-70-C-1277 Boeing

1971

17 An Investigation of the Feasibility of a Common Boundary Later Control System for High-Lift and Low-Drag on an Airfoil Section by Sean C. Roberts Miss. State Univ.

Jun 1966

18 Research Report No. 66 (USAAVLABS TR 66-36) Flight Evaluation of a Distributed Suction High-Lift Boundary Layer Control System on a Modified L-19 Liaison Aircraft Contract# DA 44-177-AMC-265(T) Miss. State Univ.

May 1966

19 STOL Report Issue 2 Fairchild Hiller Aircraft Division Apr 1966 20 Executive STOL from FLYING Mar 1962 21 Breguet STOL Transport 941 Photo Booklet Undated 22 New-Generation Airlifter (YC-14) Brochure Boeing Undated 23 deHavilland High Lift Vol.2, No.2 Feb-Mar 1978 24 STOL Airplanes – A New Approach to Air Transport by

R.A. Darby Fairchild Aircraft Division Nov 8 1955

25 AMST: Tactical Airlift Into the 21st Century (YC-14) Boeing

Undated

26 ASE 700837 Designing the OV-10A Forward Air Control and Light Attack Aircraft by Jack E. Wagner & Richard J. Arnold North American Rockwell Corp.

Oct 5-9 1970

27 Breguet 941 Manufacturer’s Model Specification Jan 15 1962 28 Breguet 941/942 Photos and Brochure Undated 29 Breguet 941S (942) Data and Drawings Undated 30 Breguet 941 Brochure Jun 1959 31 Report No. 9732 Model 188E (Breguet 941) STOL Assault

Transport with Takeoff and Payload Slide-rule May 24 1963

32 ASE S259 The Lockheed BLC Hercules – A Practical STOL Transport (with Specs. And Photo of C130B) by F.N. Dickerman & C.F. Branson Lockheed- Georgia

Nov 1 1960

33 AIAA Paper No. 71-993 Factors in STOL Flight Control Configuration by William P.A. Harris Boeing

Oct 25-28 1971

34 Autogiro Articles 1990-1994 35 SAE 960C Determination of Breguet 941 STOL Aircraft

Transition Velocities with Various Flap Settings by Harlan D. Fowler

Jan 11-15 1965

36 Report PDP-15 GL-200 STOL Army Utility Transport Lockheed-Georgia

Jan 16 1959

37 Report 43176 Small Armed Reconnaissance Aircraft D­855 Douglas Aircraft

Nov 24 1962

38 Proposal for Converting the Ryan VZ-3RY Aircraft into the Fowler System for Comparative V/STOL Flight Performance Data by Harlan D. Fowler

Aug 1954

39 A VTOL Airplane for Commercial Uses Allison 250 HP by Harlan D. Fowler

Nov 10 1960

162

40 NASA TN D 4489 Large-Scale Wind-Tunnel Tests of an Airplane Model with Two Propellers and Rotating Cylinder Flaps

Mar 1968

41 NASA CR 2135 Flight Tests of a Rotating Cylinder Flap on a North American Rockwell YOV-10 Aircraft

Nov 1972

42 Research Report No. 19 Practical High Lift Systems Using Distributed Boundary Layer Control by J.J. Cornish III Miss. State Univ.

Jan 26-29 1959

43 USAAVLABS TR 70-37 XV-11A Flight Test Program Feb 1971 44 Development of Distributed Suction High-Lift STOL

Aircraft by Sean C. Roberts Miss. State Univ. Nov 16 1965

45 ER No. 235 Evaluation of Deflected Slipstream Configurations Utilizing Boundary-Layer Control Progress Report for Aug 1956 Contract# DA 44-177-TC-370 Univ. of Wichita

Sep 1956

46 ER No. 255 Evaluation of Deflected Slipstream Configurations Utilizing Boundary-Layer Control Progress Report for Nov1956 Contract# DA 44-177-TC-370 Univ. of Wichita

Dec 1956

47 ER No. 261 Evaluation of Deflected Slipstream Configurations Utilizing Boundary-Layer Control Progress Report for Dec 1956 Contract# DA 44-177-TC-370 Univ. of Wichita

Jan 1957

48 ER No. 268 Evaluation of Deflected Slipstream Configurations Utilizing Boundary-Layer Control Progress Report for Mar 1957 Contract# DA 44-177-TC-370 Univ. of Wichita

Apr 1957

49 Delay of the Stall by Suction Through Distributed Performations by A. Raspet, J.J. Cornish III & G.D. Bryant Miss. State Univ.

Jan 23-26 1956

50 STOL Articles Various 51 Progress Report from Nov 1 1958 to Dec 31 1958

Contract# Nonr 978(01) Jan 5 1959

52 Examination of Some of the Problems Involved in the Design of Propeller-Driven Vertical-Take-Off Transport Airplanes by M.O. McKinney, R.E. Kuhn & J.B. Hammack NACA

Jan 23-26 1956

53 Some design Problems of Tilt Wing VTOL Aircraft by W.Z. Stepniewski Vertol

Oct 4 1957

54 NASA Memorandum 1-16-59L Semiempirical Procedure for Estimating Lift and Drag Characteristics of Propeller-Wing-Flap Configurations for Vertical-and-Short-take-Off­and –Landing Airplanes

Jan 1961

55 NASA TN D-5742 Large-Scale Wind-Tunnel Tests of an Airplane Model with Four Propellers and Rotating Cylinder Flaps

Apr 1970

163

56 NASA TN D-1430 Longitudinal Trim Characteristics of a Deflected Slipstream V/STOL Aircraft During Level Flight at Transition Flight Speeds

Oct 1962

57 NASA TN D-1891 Some Flight Characteristics of a Deflected Slipstream V/STOL Aircraft

Jul 1963

58 ASE 700811 Synthesis of Future High Lift Systems by Richard Scherrer Lockheed-California

Oct 5-9 1970

VTOL/GETOL GROUND EFFECTS 84 1 Report No. 203-P-1 Proposal for Test Evaluation of a

Flying Platform for the Individual Soldier by E. K. Liberatore

Feb 6 1958

2 GETOL Presentation Charts General Dynamics May 1963 3 Symposium on Ground Effect Phenomena Princeton Univ. Oct 21-23 1959 4 Ground Effect Vehicles – Photos and Articles Various 5 TR 011-2 Static Stability of Ground Effect Machines –

Thick Jet Theory by J.D. Lin Contract# Nonr-3189(00) Jun 1 1961

6 NASA TN D-660 Effects of Various Arrangements of Slotted and Round Jet Exits on the Lift and Pitching-Moment Characteristics of a Rectangular-Base Model at Zero Forward Airspeed

Feb 1961

7 NASA TN D-756 Effects of Geometric Variations on Lift Augmentation of Simple-Plenum-Chamber Ground-Effect Models

Apr 1961

8 AFFDL-TR-72-87 A Study of Air Cushion Landing Systems for Recovery of Unmanned Aircraft

Jul 1972

9 Aero Report 923 Theory of the Annular Nozzle in Proximity to the Ground

Jul 1957

10 Report No. 349 Design of Wing Sections for Use Near the Ground by T. Strand & J.J. Brainerd Air Vehicle Corp. Contract# Now 64-0349-f

Mar 1965

11 Report No. 208A90-1 On the Aerodynamic Design of Propellers and Duct Systems for Ground Effect vehicles Contract# DA 44-177-TC-524

Jan 15 1962

12 Aero Report 947 Preliminary Study of the Hovering Performance of Annular Jet Vehicles in Proximity to the Ground

Aug 1958

13 Aero Report 954 Comparison of Experimental and Theoretical Design Parameters of a 6-inch-diameter Annular Jet Model with a Jet Angle of -45o Hovering in Proximity to the Ground; and Experimental Results of Forward Flight at Zero Angle of Attack

May 1959

14 Report No. AR 581-R Aerodynamic Theory of the Annular Jet Part I Contract# Nonr-2398(00) and Nonr-2747(00)

Dec 1958

15 NASA TM X-67876 A Nuclear Powered Air Cushion Freighter for the 1980’s

Oct 17-21 1971

164

16 Report No. NA 59H-715 Analysis of NAA Tests of ground-Effect machine Concept North American

Jan 8 1960

17 IAS Proceedings Hydrofoils and Air Cushion Vehicles Sep 17-18 1962 18 SAE 133A Basic Principles of Air Cushion Vehicles by

Gabriel D. Boehler Aerophysics Company Jan 11-15 1960

19 Forward Flight Characteristics of Annular Jets by Garriel D. Boehler Aerophysics Company

Oct 21-23 1959

20 Aero Report 966 Report 1371 A Preliminary Design Technique for Annular-Jet Ground-Effect Machines (GEM’S) TED No. TMB AD-3242

Sep 1959

21 SAE 508A Some Aerodynamic Aspects of the Ground Effect by Phillippe Poisson-Quinton & Amedee Bevert

Apr 3-6 1962

22 SAE 700840 Navy Application of the ACV to Amphibious Operations by Melvin W. Brown

Oct 5-9 1970

23 IAS Preprint No. 832 The Flying Platform as a Research Vehicle for Ducted Propellers by Alvin H. Sacks Hiller Helicopters

Jan 27-30 1958

24 IAS Hydrofoil Transmissions by Eugene E. Shipley General Electric

Sep 18 1962

25 Report No. NADC-ED-L6326 Nondimensional Analysis and Parameter Optimization of Over-Water Ground Effect Vehicle types Including Aerodynamic and Wave drag Effects Contract# WEPTASK R360FR 102/2021/R011-01­001

Aug 29 1963

26 TCREC TR 62-28 An Experimental Investigation of the Response Characteristics of Two Man-Carrying Ground Effect Machines Contract# DA 44-177-TC-733

Apr 1962

27 Report GD/C-62-288 GETOL Multibased VP Concept Sep 1962 28 NASA TN D-119 Investigation of a High-Speed Hydrofoil

with Parabolic Thickness Distribution Nov 1959

29 Wing-In-Ground Effect Technology Workshop Proceedings

Sep 19-20 1978

30 Report No. 464 Longitudinal Stability and Control of a Ducted-Rotor Flying Platform by Joseph J. Trayber Contract# DA 44-177-TC-392 Princeton Univ.

May 1959

31 Convair VTOL/GETOL ZP-60-00001 (March) C.A. 1960 32 Report No. ZP-296 Convair VTOL/GETOL Logistic

Transport Vehicle Feb 28 1960

33 ADC Report No. 520-3/R24/46 Aerial Jeep Phase I Final Report Volume I of II Contract# DA-44-177-TC-397

Dec 1 1957

34 ADC Report No. 520-3/R24/46 Aerial Jeep Phase I Final Report Volume II of II Contract# DA-44-177-TC-397

Dec 1 1957

35 The Dynamic Interface Vehicle Lockheed – California Aug 1963 36 Report LR 22620 Propulsion Study for STOL Air-Sea

Craft Contract# ONR NR212-191/8-168 Code 461 Jun 29 1969

165

37 IAS Paper No. 59-121 Ground Proximity: A Critical Review by G.B. Matthews & J.L. Wosser ONR

Jun 16-19 1959

38 Aerophysics Report No. 520-2/R40/46 Aerial Utility Vehicle Monthly Progress Report for Oct 1958 Contract#DA 44-177-TC-397

Nov 6 1958

39 SBD Report No. 59-26 Aerial Utility Vehicle Monthly Progress Report for Mar 1959 Contract# DA 44-177-TC­397

Apr 3 1959

40 SBD Report No. 59-32 Aerial Utility Vehicle Monthly Progress Report for Apr 1959 Contract# DA 44-177-TC­397

May 6 1959

41 SBD Report No. 59-49 Aerial Utility Vehicle Monthly Progress Report for Jun 1959 Contract# DA 44-177-TC­397

Jul 10 1959

42 SBD Report No. 59-60 Aerial Utility Vehicle Monthly Progress Report for Aug 1959 Contract# DA 44-177-TC­397

Aug 12 1959

43 PESCO Aerial Jeep Study Proposal Feb 1958 44 PESCO “FLEEP” Phase I – Study Program Proposal Mar 1958 45 NASA TN D-1234 Force-Test Investigation of a Model of

an Aerial Vehicle Supported by Four Unshrouded Propellers

Apr 1962

46 NASA TN D-1235 Flight-Test Investigation of a Model of an Aerial Vehicle Supported by Four Unshrouded Propellers

Apr 1962

47 WASP by T.L. Metzgar 1987

VTOL FIGHTERS 85 1 XBQM-108A Papers, Articles and Photos Various

2 WADC TR 59-357 Survey and Study of VTOL-STOL Stability and Control Characteristics

Aug 1959

3 Report No. NADC-ED-5822 Study of Stability and Control of VTOL Aircraft

Jun 5 1959

4 Ryan X-13 “Vertijet” – Article and Specifications Jun 1977 5 Report 4697 Remotely Piloted Vehicle/Vertical Take-Off

and Landing Demonstration Vehicle by Warren H. Eilertson

Aug 1975

6 NARPV 75 Proceedings Jun 2-4 1975 7 Report No. 11254-1 VTO High Altitude Visual Fighter,

Ryan Model 112 Stability and Control Report Feb 13 1957

8 Report No. 11255-1 VTO High Altitude Visual Fighter, Ryan Model 112 Stabilization System Report

Sep 30 1956

9 Report No. 11518-3 Dispersed Site Fighter Bomber Ryan Model 115 Airplane Design Summary Report

Nov 26 1956

10 Report 10707 Vertical Take-Off Fighter Design Study Contract# AF 18(600)-1232

Aug 1955

166

11 Report No. 8457-3 Summary Report Jet Reaction Control Development Contract# AF 18(600)-1157

Jul 15 1955

12 Report ZP-108 Summary Report – Preliminary Design Study VTOL Day Fighter Contract# AF 33(616)-2313 Convair

Jul 30 1954

13 Report ZA-237 Estimated Stability and Control of a VTOL Day Fighter Powered by a Turbofan Engine Contract# AF 33(616)-2313

Jul 30 1956

14 Report 11518-4 Dispersed Site Fighter Bomber Ryan Model 115 Development Plan Contract# AF 18(600)-1641

Nov 1956

15 Report No. 10441-12 Interim Progress Report – Advanced Jet Reaction Control Development Contract# NOa(s)­10035

Dec 31 1956

14 Report No. ZW-038 VTOL Day Fighter – Preliminary Weight and Balance Report Contract# AF 33(616)-2313

Jul 30 1954

15 Report No. 39.50.41 Final Summary Report – Design Study of a VTOL Dayfighter Aircraft Powered by a Turbo-Fan Engine Contract# AF33(616)-2314

Jun 15 1954

16 Report No. LR 10707 Summary Report Vertical Take-Off Fighter Design Study Lockheed-California

Aug 1955

17 Report No. 11518-2 Program Summary Report – Dispersed Site Fighter-Bomber Study Ryan Model 115

Nov 30 1956

18 Report No. 8452-1 Final Report – VTO Fighter Design Study Contract AF18(600)-1157

Jul 15 1955

VERTICAL LIFT RESEARCH / WINGLESS AIRCRAFT

86 1 Report X-475 Proposal for a Hot Cycle Compound Helicopter Feasibility Program plus Cover Letter HTC

Jul 1960

2 Report No. 159-5 Aerodynamic Analysis Model 159 Convertiplane AHC

Dec 15 1950

3 The TRW Approach to Complete Assessment of the Cheyenne by John F. Mosher TRW

C.A. 1967

4 Operating Problems and Experience with the Sikorsky Skycrane by Miller A. Wachs Sikorsky

1967

5 K-16B reports List 1956-1965 6 AFFDL-TR-67-93 Effects of Gust Velocity Spatial

Distributions on Lateral-Directional Response of a VTOL Aircraft

Jun 1967

7 The Challenge of Aerial Systems Analysis by LTG William B. Bunker

Undated

8 Operational Problems and Experience with Vertical-Lift Aircraft Light and Utility Helicopters by John W. Oswalt

Nov 15 1967

9 Dynamic Analysis in Weapons System Design and Evaluation by Carl V. Swanson

Undated

167

10 The Analog Approach to Aerial Weapon Systems Analysis by William J. Kenneally

Undated

11 Technical Paper No. 309 Some Performance and Weight Aspects of the GETOL Transport by W.Z. Stepniewski & A.H. Schmidt Boeing-Vertol

May 14-17 1962

12 SAE 624A The T65 and T72 Shaft Turbines by I.W. Nichol

Jan 14-18 1963

13 Zeitschrirt Fur Flugwissenschaften – article about Claudius Dornier (in German)

May 1964

14 Maneuverable Long Line Loiter System (MALLLS) – Miscellaneous Articles and Slides

Undated

15 Computation of Rotary Wing Harmonic Airloads and Comparison with Experimental Results by Raymond A. Piziali & Frank DuWaldt

May 2-4 1962

16 Experimental Research on 4-Duct Tandem VTOL Aircraft Configurations by M.O. McKinney & W.A. Newsom NASA Langley

May 3-5 1962

17 Design and Test of a Helicopter Turbine Inlet Foreign Particle Separator by R. Hooper & D.A. Richardson Boeing-Vertol

Undated

18 A Review of Low Airspeed Measurement Techniques by John Leak Boeing-Vertol

Undated

19 Observations on Subsonic V/STOL Aircraft Designs by Bernard Lindenbaum

Jun 30 1960

20 SAE 266G Mass TRANSPORTATION BY High-Speed VTOL by H.V. Borst & J.M. Mergen Curtiss

Jan 9-13 1961

21 A Generalized Experimental Study of Inlet Temperature Rise and near Field temperature Contours of Jet V/STOL Aircraft in Ground Proximity by Robert F. Speth & Patrick E. Ryan Bell

Undated

22 SAE 670352 Turbofan/Turboshaft Powerplant for Composite Helicopters by W.O. Gaffin & S.E. Wilcox Pratt and Whitney

Apr 24-27 1967

23 SAE 660763 Multiroller Planetary Friction Drives by Algirdas L. Nasvytis TRW

Oct 17-21 1966

24 Report No. R-849 Remote Flight Delivery System Concept Presentation Kaman

Apr 20 1970

25 Remote Retrievable Parapoint for Special Operations Sep 1987 26 AMRL-TR-69-140 Long-Line Loiter: Personnel Retrieval

System Mar 1971

27 AMRL-TR-70-104 Long Line Loiter: Personnel retrieval System : Triaxial Acceleration Tests

May 1972

28 AMRL-TR-71-85 Long Line Loiter: Psychological Warfare Package

Jul 1971

168

29 Report PDR-306-II Surface-to-Air Retrieval of Heavy Spacecraft by Fixed-Wing Aircraft Volume II – Development of Analytical Techniques Contract# NAS9­195

Jun 1962

30 A Preliminary Design of a Remotely-Controlled Glider for a Long-Line Operation – Thesis by 1LT Eldridge L. Snapp III USAF

Jun 1979

31 Report No. R-407 10-Ton Intra-Theater Transport Kaman Jul 11 1962 32 Piasecki Model 16H Compound Helicopter Proposal 1962 33 Some Basic Derivations About the Action of a Shrouded

Propeller Collins Jul 16 1956

34 Report CER-924 Preliminary ER on the .4 Scale Aerodyne Model Static Tests Collins

Feb 1959

35 Report No. CER-1014 Final Report on Research on Wingless Aircraft Contract# NOnr-2566(00)

Jul 1 1959

36 Report No. CER-1045 Part I Lift-Thrust Data Analysis for a Wingless Aircraft Model (Mark V) Contract# NOnr 2557(00)

Aug 1 1959

37 Report No. CER-1045 Part II Lift-Thrust Data Analysis for a Wingless Aircraft Model (Mark V) Contract# NOnr 2557(00)

Aug 1 1959

38 Report No. CER-1045 Part II Lift-Thrust Data Analysis for a Wingless Aircraft Model (Mark V) Contract# NOnr 2557(00)

Aug 1 1959 rev Jan 15 1960

39 Report No. CER-1045 Part III Lift-Thrust Data Analysis for a Wingless Aircraft Model (Mark V) Contract# NOnr 2557(00)

Jan 31 1960

40 SAE 747C An Economic Assessment of the Hot Cycle Compound Helicopter for VTOL Transport by Malcolm Harned & Harvey O. Nay HTC

Sep 23-27 1963

41 Ejector Shroud Articles (7) Undated 42 NACA RM L55F28 An Experimental Investigation of a

Flat Ram-Jet Engine on a Helicopter Rotor Jan 4 1956

43 Report ER 4221 New Light Observation Aircraft Lockheed-Georgia

Feb 1 1960

44 Report 2-Y-2 Wind Tunnel Tests of ¼-Scale Model of PiAC VTOL Aircraft PA-2C Contract# NOa(s)56-834-c

Jan 5 1959

45 Report 2-Y-4 Ring-Wing V/STOL Logistics Aircraft Contract# ARDC-SR No. 175

Feb 25 1960

46 XV-1 Flight Safety Inspection Jun29-Jul 1 1954 47 NACA TN 4117 Experimental Investigation of Lift, Drag,

and Pitching Moment of Five Annular Airfoils Oct 1957

48 Report No. RAC 651-901A VTOL/STOL Logistics Aircraft Parametric Study 1965-1970 Time Period Republic

Feb 19 1960

169

49 Report 57-59 1031-B Wind Tunnel Model Specification and Tunnel Program Hiller

Jun 3 1957

50 Report NA-62-954 Ten Ton Assault Transport NAA Aug 29 1962 51 Recollections- Chapter 5 Wright Field and Aircraft

Laboratory WWII 1941-1945 by Dr. Courtland Perkins C.A. 1989

52 TR D3-3512-1 Human Reaction to Low Frequency Vibration Contract# NONR 2994(00) Boeing

Undated

53 Miscellaneous Papers 1953-1956

DOWNWASH AND GROUND EFFECT 87 1 Symposium on Ground Effect Phenomena Princeton Univ. Oct 21-23 1959

2 WADD Technical Note 60-183 Hot Gas Surface Erosion Studies

Aug 1960

3 Report No. FDDS-67-6 Test Report on Measurements for V/STOL Vehicle Downwash Characteristics

Sep 22 1967

4 USAAVLABNS TR 68-52 Investigation of the Downwash Environment Generated by V/STOL Aircraft Operating in Ground Effect Contract# DA 44-177-AMC-316(T)

Jul 1968

5 Kellett Downwash Contract# Now 61-0926-C C.A. 1963 6 Report No. 179T80-2 An Investigation of VTOL

Operational Problems Due to Downwash Effects Contract# Now 60-0450-f Kellett

Jun 12 1961

7 Report No. 179T80-6 Effects of Airframe Geometry on Downwash Problems of Tandem Ducted-Propeller VTOL Aircraft Contract# Now 61-0926-c

Jan 1964

8 Report No. 179T80-12 Downwash Tests of the Dual tandem Ducted Propeller VTOL Research Aircraft Configurations to Evaluate Single Inlets, Protection Devices and Study Aerodynamic Interference Kellett

Nov 1 1965

9 Report No. 2023-917001 VTOL/STOL Flying Handling Qualities Specification Study Contract# NOas 60-6067-f Bell

Jun 25 1960

10 WADC TR 59-357 Survey and Study of VTOL-STOL Stability and Control Characteristics

Aug 1959

11 NASA TN D-4624 Study of Optimum Values of Several Parameters Affecting Longitudinal Handling Qualities of VTOL Aircraft

Jul 1968

12 Report No. 484 Theoretical Investigations Related to Unsteady Air Forces on Wing/External Store Combinations of VTOL Aircraft by J. Becker & A. Lotze (From German)

Nov 20 1969

13 Report No. 012-26 An Investigation of the Over Water Aspects of VTOL Airplanes at High Disc Loading Contract# Now 62-0279-d Curtiss

Dec 1963

170

14 AHS 28th Annual National Symposium Paper 642 An Experimental Investigation of STOL Longitudinal Flying Qualities in the Landing Approach Using the Variable Stability X-22A Aircraft by J.M. Schuler, R.E. Smith & J.V. Lebacqz Cornell

May 1972

15 AHS 28th Annual National Symposium Paper 644 A Pilot’s Opinion: VTOL Control DesignRequirements for the Instrument Approach Task by James M. Patton, Jr. NASA Langley

May 1972

16 AHS 28th Annual National Symposium Paper 654 An Integrated System of Airborne and Ground-Based Instrumentation for Flying Qualities Research with the X­22A Airplane by John L. Beilman Cornell

May 1972

17 AIAA Paper No. 64-777 Handling Qualities of VTOL Aircraft by Richard K. Wilson & Charles B. Westbrook AF Flight Dynamics Lab, WPAFB

Sep 21-23 1964

18 AGARD Flight Mechanics Panel (27th Meeting) Application of the Model Technique to a Variable-Stability Helicopter for Simulation of VTOL Handling Qualities by John F. Garren, Jr. & James R. Kelly NASA Langley

Oct 11-12 1965

19 Analysis of a Jet in a Subsonic Crosswind NASA Symposium

Sep 9-10 1969

20 Report No. CAL NO. 171 An Experimental Study of Pilot Visibility from a VTOL Aircraft in Overwater Hover Contract# N00014-68-C-0241 NR 212-182 Cornell

Apr 1969

21 Recirculation Model Tests (condensed paper) by Felix Aulehla (stamped 5)

Jan 15 1970

22 V/STOL Technology Briefing 1970 (Stamped 4) Jan 15 1970 23 Handling Qualities and Pilot Dynamics by Charles B.

Westbrook WADC & Duane T. McRuer Systems technology, Inc from Aero/Space Engineering

May 1959

24 Stabilisation en vol Vertical Des Avions VTOL by G. Ernst & J. Jardinier SNECMA (in French)

Jun 1960

25 Standard Flight Control Systems for Aircraft designed at Present in the Federal Republic of Germany, incl. VTOL

Undated

26 NASA TN D-977 An Investigation of the Downwash from a VTOL Aircraft and a Helicopter in the Ground Environment

Oct 1961

27 NASA TN D-5175 An Investigation of a Direct Side-Force Maneuvering System on a Deflected Jet VTOL Aircraft

Apr 1969

28 NASA TN D-5617 Review of Propulsion-Induced Effects on Aerodynamics of Jet VTOL Aircraft

Feb 1970

29 NASA TN D-5729 An Exploratory Wind-Tunnel Investigation of the Wake Effect of a Panel Tip-Mounted Fan-Jet Engine on the Lift-Induced Vortex

May 1970

171

30 AFFDL-TR-68-69 Study and Simulation Program to Investigate the Mechanization of an Aircraft Flight Control System that Employs Direct Lift Volume I: Preliminary Design of Direct Lift Controls

Jun 1968

31 Bad Weather Landing of VTOL Aircraft by Dr. K.H. Fischer (from German)

Mar 1970

32 A Review of AGARD Recommendations for V/STOL Handling Qualities (Report 408) in the Light of US Army Experience with the XV-5A and Other V/STOL Aircraft Including Helicopters by US Army Test & Evaluation Command

Undated

33 VTOL Six Degree of Freedom Control System Colt Industries

Undated

34 Report No. 214-100-59 Aero-Thermo Requirements for ESA 4209 NAA

Sep 11 1959

35 Report No. 210-98-59 V/STOL Simulation Scheduling and Utilization NAA

Oct 27 1959

36 Report No. 210-102-59 Analysis of V/STOL Wind Tunnel Testing Requirements NAA

Nov 11 1959

37 Report No. 214-3-60 A Note on Stability and Control Problems of VTOL Aircraft in Hovering and very Slow Flight NAA

Jan 11 1960

38 Simulator Photos (2) May 25 1966 39 SAE 700785 A Fluidically-Augmented Artificial Feel

System for High Performance Aircraft by Tor W. Jansen & Walter W. Kaniuka NADC

Oct 5-9 1970

40 Downwash in Connection with Rescue Papers, Letters & Notes

C.A. 1968

41 AHS 24th Annual National Symposium Paper 204 Avionics and Armaments Panel Session

May 8-10 1968

42 AHS 24th Annual National Symposium Paper 219 VTOL Handling Qualities Crireria and Control Requirements – Analysis and Experiment by Thomas E. Lollar & Gerhard K.L. Kriechbaum Boeing

May 8-10 1968

43 AHS 26th Annual National Symposium Paper 444 Models for a VTOL Airplane in Transition by David L. Key Cornell Aero Labs

Jun 1970

44 VTOL Control/Stability Articles (3) 1962-1965 45 Report No. 179T80-11 Interim Report on Tests of Engine

Injection of a Full-Scale Reflection Plane Model of the Ducted Fan Tandem VTOL Research Aircraft Kellett

Jul 17 1964

46 Report No. DCR-268 Downwash Environment for the Boeing Model 160 V/STOL Aircraft Dynasciences

Jan 1968

47 Report No. D6-9908 Design Surface temperatures for V/STOL Aircraft Boeing

Jan 30 1964

48 Applied Aerodynamics for V/STOL Northrop Mar 1970

172

49 Study of Application of Pure Fly-By-Wire Primary Flight Control Systems to Propeller Driven V/STOL Aircraft Curtiss-Wright

Sep 13 1965

50 Report No. NOR 67-135 VTOL Aircraft Reaction Control Technology Studies Northrop

Jun 1967

51 Report No. NA61H-804 An Analytical Study of the Dynamic response of V/STOL Vehicles NAA

Dec 21 1961

VTOL PROPOSALS/CONCEPTS 88 1 Report No. C-2842 Summary Flight Test Report on the

Curtiss-Wright X-100 VTOL Aircraft Nov 30 1960

2 Report No. SD-139A Curtiss-Wright High-Speed VTOL Aircraft Model 200 General Configuration and Performance

Mar 1961

3 Report No. PDA-70461 Curtiss-Wright VTOL Aircraft for Air Force Recovery Missions

Jul 3 1961

4 Report No. C-2798 Design and Performance of the Lifting Propeller X-100 VTOL Airplane Curtiss

Oct 8 1959

4 Presentation to AFSC V/STOL Aircraft Curtiss Oct 18 1963 5 Curtiss-Wright High-Speed VTOL C.A. 1963 6 Report No. 014-252 X-19 Aerodynamic Stability and

Control Summary Curtiss Feb 19 1964

7 AFFTC TR 66-27 X-19 Category I Limited Flight Evaluation

Oct 1966

8 Glass Fiber Reinforced Plastic Blades Brochure Curtiss 1961 9 Curtiss-Wright High Speed VTOL Brochure (3) Undated 10 AFSC System 664A System Package Program – X-19

VTOL Research Aircraft Mar 15 1965

11 Development of the Curtiss-Wright V/STOL Airplanes by Henry V. Borst Borst Assoc.

Undated

12 VTOL The Significance of Radial Force Pamphlet Curtiss Undated 13 Report No. 014-523 Stability and Control Analysis of X-19

Flight Testing for Flights 2 Through 22 Curtiss Dec 31 1964

14 Report No. 014-731 X-19 power Required Derived From Category I Flight test Results Curtiss

Dec 3 1965

15 Blueprints of M-260 Recovery Vehicle Curtiss Jun 27 1961 16 Report of X-19 VTOL Program Technical Review (2) Jan 1965 17 The High-Speed VTOL X-100 and M200 Aircraft by H.V.

Borst Curtiss Aug 1962

18 Can the Osprey Survive in Combat? An Assessment of MV-22 Combat Effectiveness by Maj.George J. Trautman, III USMC Naval War College

Feb 16 1988

19 AIAA Paper 63-483 The Domain of the Convertible Rotor by R. Hafner Westland Aircraft Ltd.

Oct 21-24 1963

20 Verticraft Corporation Lift-Fan Aircraft – Photos and Drawings

1961

173

21 Malvestuto Proposal – Documents, Drawings, Presentations

1969

22 Malvestuto Proposal Presentation C.A. 1969 23 Curtiss-Wright X-19 Miscellaneous Photos & Articles C.A. 1962 24 NASA TN D-1239 An Experimental Study of the Effect of

Downwash from a Twin-Propeller VTOL Aircraft on Several Types of Ground Surfaces

May 1962

25 Letters to Hon. F.C. Carlucci re: JVX 1982 26 WFG-P16 & P23 (in German) Undated 27 Investigation of Change in Horsepower with Early

Transitions from Propeller Mode to Helicopter Mode with Handwritten Notes. Sikorsky

Undated

28 Rotavion, Inc – Correspondence and Notes C.A. 1960 29 Report XR-62 VTOL Aircraft Votavion, Inc 1961 30 Report No. PR-4 Proposal for a Flight test Program on the

Vanguard 2 Fan-In-Wing VTOL/STOL Aircraft Feb 23 1960

31 Report No. T-2-T Tie-Down Tests of the Vanguard Model 2 Fan-In-Wing VTOL Aircraft

Nov 28 1959

32 Vanguard Model 2 – Miscellaneous Photos and Papers C.A. 1960 33 Report No. PR-106 Proposal for the Advancement of

Techniques for V/STOL Lift and Propulsion Systems Vanguard Corp.

Aug 31 1961

34 Report 28-X-1 SR-175 Study Report – VTOL/STOL Logistics Aircraft A Parametric Study for the 1965-1970 Time Period Vanguard Corp.

Feb 23 1960

35 Report No. PR-4(2) Proposal for the Continuation of test program on the Vanguard 2 Fan-In-Wing VTOL/STOL Aircraft

Apr 8 1960

36 Vanguard Model 2 Miscellaneous Correspondence and Proposals

C.A. 1960

37 Vanguard Model 2C Tests Ames Research 1962

TILT WING AIRCRAFT 89 1 Report No. TS-152 Type Specification for Tri-Service

VTOL Prototype Transport Aircraft Jan 13 1961

2 Tilt Wing VTOL Aircraft – Sketches & Charts Undated 3 VC 400 VTOL Cargo Aircraft by Dr. Siegfried Gunter

VFW Munchen Jun 1966

4 Report No. D8-2076 Evaluation of Geared Flap Control System for Tiltwing V/STOL Aircraft Boeing Co.

Aug 11 1970

5 Tilt Wing Proposal and Papers Boeing Aircraft Co. May 18 1967 6 AIAA Paper No. 71-992 A Comparison of Outflows from

a Helicopter, Tilt-Wing and Jet Lift Hovering Aircraft by Odd E. Michaelsen Canadair

Oct 25-28 1971

174

7 AFFDL-TR-70-124 Detail Design of Critical Components for a Prop/Rotor Aircraft Final Report, Phase II Boeing-Vertol

Jul 1970

8 ASD-TR-69-15 Propeller Static Performance Tests for V/STOL Aircraft

Jan 1970

9 NASA TN D-946 Rapid-Transition Tests of a 1/4 – Scale Model of the VZ-2 Tilt-Wing Aircraft

Oct 1961

10 NASA TN D-989 Summary of Flight test results of the VZ-2 Tilt-Wing Aircraft

Feb 1962

11 NASA TN D-1365 Longitudinal Stability and Control of a Tilt-Wing VTOL Aircraft Model with Rigid and Flapping Propeller Blades

Jul 1962

12 NASA TN D-1375 Flight Test Investigation of Ailerons as a Source of Yaw Control on the VZ-2 Tilt-Wing Aircraft

Jun 1962

13 NASA TN D-1389 Force-Test Investigation of the Stability and Control Characteristics of a Four-Propeller Tilt-Wing VTOL Model with a Programmed Flap

Sep 1962

14 NASA TN D-1390 Flight Investigation of the Longitudinal Stability and Control Characteristics of a Four-Propeller Tilt-Wing VTOL Model with a Programmed Flap

Sep 1962

15 NASA TN D-2680 Flight Investigation of the VZ-2 Tilt-Wing Aircraft with Full-Span Flaps

Mar 1965

16 NASA TN D-4030 Aerodynamic Data on Large Semispan Tilting Wing with 0.5-Diameter Chord, Single-Slotted Flap, and Single Propeller 0.08 Chord Below Wing

Jul 1967

17 NASA MEMO 1-16-59L Semiempirical Procedure for Estimating Lift and Drag Characteristics of Propeller-Wing-Flap Configurations for Vertical-and Short-Take­Off-And-Landing Airplanes

Dec 1958

18 Report No. 478 A Stability Analysis of Tilt-Wing Aircraft by Henry E. Payne III & Charles H. Cromwell III Princeton Univ.

May 1960

19 Tilt-Wing Applications by Blaine R. Parkin General Dynamics & Saul Bernstein Canadair

Undated

20 Vertol MOCO (Monocyclic Control)Programs 1966 21 Flight Test Experience of a Tilt Wing VTOL by W.Z.

Stepniewski Vertol Jun 15-18 1959

22 Report No. PR-543 Monocyclic Control Program (MOCO) Revision A

May 28 1965

23 Proposal to Test a Simplified Tilt-Wing with MOCO (Appendices)

Dec 1965

24 Report No. PR-394 Proposal – Boeing-Vertol 119F Tilt-Wing Aircraft

Undated

25 Report No. D8-2369-4 V/STOL Propeller Design Parameters Boeing

Apr 1969

26 MBB GMBH BO-140 V/STOL Transport Nov 1969

175

27 Grumman Design 242 Tri-Service Transport Pamphlet Apr 17 1961 28 Grumman Design 170a Tilt-Wing Rescue Aircraft Dec 21 1959 29 Grumman design 134E VTOL Mohawk Jan 1959 30 Conclusions and Recommendations for XC-142A Undated 31 Requirements for Automatic Stabilization of the XC-142A

in the V/STOL Flight Modes Chance-Vought 1963

32 Report No. 2-51072/2R6A detail Specification for Model XC-142A VTOL Cargo Assault Aircraft Contract# AF 33(657)-7868 Chance Vought

Oct 4 1963

33 XC-142A V/STOL Transport Transmission System Brochure Hiller Vought Ryan

Undated

34 Report No. 56-61 Tilt Wing Propelloplane Selection and Optimization for Transport – Rescue Missions Hiller

Jun 1956

35 Report No. AER-E1R-13347 VHR-447 Tri-Service Transport Vol.7 Summary Report Part 2 Airplane Description Hiller Vought Ryan

Apr 1961

36 VTOL Amphibious Assault Transport Systems 1962-1967 Phase II Summary Report – Assault Helicopters

Nov 15 1957

SHROUDED PROPELLERS AND PROPULSION SYSTEMS

90 1 AFFDL-TR-71-88 Volume II – Advanced V/STOL Propeller Technology – Static Thrust Prediction Method Development

Sep 1971

2 AFFDL-TR-71-88 Volume V – Advanced V/STOL Propeller Technology – Surface Pressure Measurements on a Propeller Blade Operating at Zero Advance Ratio

Sep 1971

3 AFFDL-TR-71-88 Volume VI – Advanced V/STOL Propeller Technology – Small Scale Cyclic Pitch Investigation

Jun 1972

4 AFFDL-TR-71-88 Volume VII – Advanced V/STOL Propeller Technology – Large Scale Cyclic Pitch Investigation

Jun 1972

5 AFFDL-TR-71-88 Volume IX – Advanced V/STOL Propeller Technology – Advanced Materials Study

Mar 1973

6 AFFDL-TR-71-88 Volume X – Advanced V/STOL Propeller Technology – Advanced Propeller Design

Dec 1971

7 AFFDL-TR-71-88 Volume XI – Advanced V/STOL Propeller Technology – Advanced Gearbox Design

Jul 1972

8 AFFDL-TR-71-88 Volume XII – Advanced V/STOL Propeller Technology – Advanced Propeller Manufacture and Test

Apr 1974

9 AFFDL-TR-71-88 Volume XIII – Advanced V/STOL Propeller Technology – Far-Field Noise Investigation

Mar 1972

10 AFFDL-TR-71-88 Volume XIV – Advanced V/STOL Propeller Technology – Program Summary Report

Apr 1974

176

11 Report No. 213-1 Shrouded Propeller Investigations: Wind Tunnel Tests of a Shrouded Propeller with a 17-Bladed Rotor, Inlet and Exhaust Stators, and Long Shroud with High-Speed Inlet and No Exit Diffusion Contract#NONR­201(01) Univ. of Wichita

Jun 1958

12 Report No. 213-8 A Method of Design of Shrouded Propellers Contract#NONR-201(01) Univ. of Wichita

Oct 1959

13 Report No. 213-9 Shrouded Propeller Investigations: Shroud and Centerbody Pressure Distributions of a Shrouded Propeller with 17-Bladed Rotor, Inlet and Exit Stators and Long Chord Shroud Contract# NONR-201(01) Univ. of Wichita

Oct 1959

14 Report No. 213-10 Shrouded Propeller Investigations: Shroud and Centerbody Pressure Distributions of a Shrouded Propeller with 10-Bladed rotor, Exit Stators and Long Chord ShroudContract#NONR-201(01) Univ. of Wichita

Jan 1960

15 Report No. 213-11 Shrouded Propeller Investigations: Wind-Tunnel Tests of a 2-Bladed Shrouded Propeller Model Contract#NONR-201(01) Univ. of Wichita

Nov 1960

16 Report No. 213-12 Shrouded Propeller Investigations: Wind-Tunnel Tests of a 4-Bladed Propeller Model having a 0.30 Hub/Tip Diameter Ratio Centerbody Contract#NONR-201(01) Univ. of Wichita

Mar 1961

17 Report No. 213-13 Shrouded Propeller Investigations: Wind-Tunnel Tests of a 4-Bladed Propeller Model having a 0.4 Hub/Tip Diameter Ratio Centerbody Contract#NONR-201(01) Univ. of Wichita

Mar 1961

18 Report No. 213-15 Shrouded Propeller Investigations: Propeller Tip Clearance EffectsContract#NONR-201(01) Univ. of Wichita

Apr 1961

19 Report No. 337 Shrouded Propeller Investigations: Aerodynamic Characteristics of a Shroud with Centerbody Contract#NONR-201(01) Univ. of Wichita

Feb 1959

20 WADC TR 58-604 Wind Tunnel Tests of Shrouded Propellers at Mach Numbers from 0 to 0.60 Contract# AF 33(616)-5363 (Copy)

Dec 1958

21 Research Note #7 Ducted Propeller Studies at Mississippi State Univ. Contract# Nonr 978(01)

Nov 28 1958

22 Aero Report 951 Shrouded Propeller Thrust Ratio as a Measure of Shroud and Propeller Static Performance

Jan 1959

23 Document No. 70-6568(25) Investigation of a Low Loading High tip Speed Transonic Fan Stage NASA Progress Report May 29 to Jul 2 1972 Contract# NAS3­13498 Garrett

Jul 26 1972

177

24 Document No. 72-8597(4) Application of Holography to Flow Visualization within Rotating Blade Row Monthly Technical Progress Narrative Aug 27 to Oct 1 1972 NASA Contract# NAS 3-15336 Garrett

Oct 30 1972

25 Research Report No. 20 Study of a Shrouded Propeller with Distributed Suction on the Inlet Profile by Henry Marshall Claybourn, Sr. Contract# Nonr 978(01) Mississippi State Univ.

Jan 20 1959

26 Bi-Monthly Progress report No. 1 Analytical Study of Shrouded Propellers Contract# AF33(616)-2765 Longren Aircraft Co.

Feb 1955

27 Report No. ARD-224 Wind Tunnel Test of Several Ducted Propellers in Non-Axial Flow Phase IV Contract# Nonr 1357(00) Hiller

Apr 20 1959

28 Theory and Testing of Jet Propulsion Motors and Rockets by Zygmunt Fonberg Aircraft Jet and Rocket Corp.

1945

29 Propulsion – Miscellaneous Articles Various 30 SAE 650201 Lift Engine technology by T. Foster & H.D.

Paget Continental Apr 12-15 1965

31 Propulsion for VTOL GE Mar 18 1963 32 Report NO> DM 62-14 A Comparison of VTOL

Propulsion Systems in a Subsonic Mission by W.L. Rodenbaugh GE

Jan 18 1962

33 Propulsion for Army VTOL Requirements GE Undated 34 Q-Fan folder and Articles Hamilton-Standard 1972-1973 35 Report No. EDR 5584 Allison Model 501 Free Turbine

Turboshaft Engines Jan 1968

36 Propulsion Systems for Remotely Piloted vehicles GE Undated 37 Report No. D210-10696-1 Study of Extreme High Altitude

Propulsion Contract# F33657-74-C-0166 Beoing-Vertol Sep 1974

38 Report No. QFT-55-18 rev A Q-Fan Propulsion System Preliminary Specification – QFT-55-18 Hamilton-Standard

Sep 20 1971

39 Report No. QFT-55-18 rev B Q-Fan Propulsion System Preliminary Specification – QFT-55-18 Hamilton-Standard

Jun 1972

40 Report No. QFT-64-18 rev B Q-Fan Propulsion System Preliminary Specification – QFT-64-18 Hamilton-Standard

Jun 1972

41 Re-Design of a Lightweight, Low-Volume, Piston Engine Hydra-Electric Co.

May 17 1973

V/STOL FIGHTERS 91 1 V/STOL Fighter Blueprints 1963

2 10-Ton V/STOL Assault Transport Blueprints 1962 3 V/STOL Fighter Pamphlets and Overlays Various

178

4 NASA TN D-4812 Aerodynamic Characteristics of a Five-Jet VTOL Configuration In the Transition Speed Range

Oct 1968

5 NASA TN D-5727 Induced Interference Effects on the Aerodynamic Characteristics of a 0.16-Scale Six-Jet V/STOL Model in Transition

Mar 1970

6 NASA TN D-5770 Wind-Tunnel Investigation of a VTOL Jet-Transport Model with Powered Lift Engines in Pods at Wing Midspan or Inboard

Apr 1970

7 Progress Report on Fiat G 95/4 Program Presented in Rome the 13th of April

Undated

8 Proposal for T-38 ARPS V/STOL Trainer Aircraft Northrop Norair

Mar 1965

9 Society of Experimental Test Pilots – Mach 2 V/STOL (VJ 101) Flight Test Program by George L. Bright

Sep 27-28 1963

10 V-465 V/STOL Transport Charts and Diagrams (incomplete)

Undated

11 Report No. 2000-910200 VTOL Fighter Program – Bell VTOL/STO-VL Airplane – Detail Specification

Dec 23 1958

12 VTOL Technology Status NAA Nov 1965 13 Tech. Memo AERO 911 Results of Flight Tests on the

Short SC1 VTOL Research Aircraft with Particular Reference to Handling Qualities in the Hover and Transition Royal Aircraft Establishment

Sep 1965

14 NAA CX-6 Study Undated 15 Report No. 2000-927007 VTOL Fighter Program –

Experimental Model Programs Contract# NOas 57-836-c Bell

Feb 6 1959

16 Report No. 2000-902058 VTOL Fighter Program – Ground Velocities and Temperatures Jet Impingement Tests (Model 2000-971111) Contract# NOas 57-836-c Bell

Jan 30 1959

17 Navy D-188A VTOL Fighter Program Presentation Bell Feb 19959 18 Document No. D2-4918 Technical Design Studies –

Interim Report Boeing Oct 8 1959

19 Document No. D2-4918-1 Supplemental Information for D2-4918, Technical Design Studies – Interim report Boeing

Oct 26 1959

20 Document No. D2-4943 Tactical Test Program – Past, Present and Future Boeing

Oct 10 1959

21 Document No. D2-5032 Tactical Design Studies – Trade Data Boeing

Oct 26 1959

22 Document No. D2-5161 VTOL/STOL Airplane – Engine matching Study Boeing

Nov 13 1959

23 Report No. D188A-945-238 Navy VTOL Fighter Program – Progress Report No. 2 Contract# NOas 57-836-c

Apr 11 1958

24 Vertical Take-Off Research Aircraft Specification No. ER.143.T Shorts Aircraft, Ltd.

Feb 1954

179

25 Report No. M42-945-001 Summary of V/STOL Tactical Fighter Investigations Bell

Jun 24 1959

26 Report No. 2000-933001 V/STOL Tactical Fighter Bell Aircraft – Convair

Oct 1 1959

27 The Design of a Supersonic V/STOL Fighter-Bomber by James A. O’Malley, Jr. Bell

Jun 14 1961

28 Report No. 2000-902058 VTOL Fighter Program – Progress Report for April 1958 Contract# NOas 57-836-c Bell

May 15 1958

29 Report No. 2000-953001 XF-109 V/STOL Tactical Fighter Weapons System Bell

Feb 17 1959

30 NACA RM SL58H15 Low-Speed Wind-Tunnel Tests of a 1/8-scale Model of the Bell D-188A VTOL Airplane

Aug 15 1958

31 Report No. D188A-945-206A Standard Aircraft Characteristics Model D188A Bell

Jan 24 1958

32 VJ 101C Pamphlet (in German) Undated 33 Report No. 2000-927006 VTOL Fighter Program –

Description and Technical Data for Mock-Up Inspection Contract# NOas 57-836-c Bell Aircraft

Feb 6 1959

34 Report No. 2000-927010 VTOL Fighter Program – Proposal Bell

Oct 1 1959

35 Report No. LR 17896 Proposal for VTOL Test vehicles Using F-104A Lockheed-California

May 28 1964

36 Report No. ER-6182 GL293 – VTOL C130 Lockheed-Georgia

Oct 1963

VTOL – GENERAL 92 1 AGARDograph 46 Symposium on Vertical & Short Take-

Off and Landing Aircraft Part I Jun 1960

2 AGARDograph 89 V/STOL Aircraft Part I Sep 1964 3 AGARD-CP-126 Military Applications of V/STOL

Aircraft Volume I Oct 1972

4 Report No. 350 Unified Performance Theory for V/STOL Aircraft in Equilibrium Level Flight Contract# Nonr­4926(00)(X) Air Vehicle

May 1966

5 Report No. FAA-ADS-26 STOL-V/STOL City Center Transport Aircraft Study Contract# FA64WA-5012

Oct 1 1964

6 Report NO. NA-63-1262 V/STOL Convictions NAA Nov 6 1963 7 Report No. ARD-182.1 Supplementary Technical Data to

High Performance Missile Resupply Aircraft May 2 1958

8 Report No. 182 Proposal for the Study of a High Performance Missile Resupply Aircraft Hiller

Jan 24 1958

9 Future of Military V/STOL Oct 4 1977 10 Report No. 553-6 (ARD 758-400) A Study of the

Comparative Effectiveness of V/STOL and STOL Aircraft in Limited and General War Environments

Oct 11 1962

180

11 Report No. R-670 Post 1980 Navy Air Rescue Presentation Kaman

Feb 27 1967

12 Report No. NADC-76019-30 Parametric and Conceptual Design Study of Small V/STOL Sea Loiter Aircraft Lockheed-California

Feb 1977

13 AFAPL-TR-66-90 An Analytical Method of Determining General Downwash Flow Field Parameters for V/STOL Aircraft

Nov 1966

14 USAAVLABS TR 67-40 Investigation of Hydraulic Power Transmission Systems for V/STOL Aircraft

Aug 1967

15 NASA TN D-862 A Flight Examination of Operating Problems of V/STOL Aircraft in STOL-Type Landings and Approach

Jun 1961

16 Ten-Ton V/STOL Transport Presentation Chance-Vought Undated 17 Tactical Employment of Brigades and Battalions of

Infantry and Mechanized Divisions by Col. Ralph L. Whitt US Army

Undated

18 Some Aspects of Convertible Aircraft Design by Robert L. Lichten Bell

May 9 1949

19 IAS No. 724 Evaluation of VTOL Systems Suitable for Transport Aircraft by W.Z. Stepniewski & Joseph Mallen Vertol

Jan 28-31 1957

20 AIAA Paper No. 71-980 The V/STOL Projects of the Federal Republic of Germany by Drury W. Wood Dornier

Oct 25-28 1971

21 Technical Paper No. 309 Some Performance and Weight Aspects of the GETOL Transport by W.Z. Stepniewski Boeing-Vertol

May 14-17 1962

22 Design Considerations for VTOL Aircraft by Edward E. Swanson & Donald W. Robinson, Jr. Kaman

Dec 11 1962

23 AHS 24th National Forum Paper No. 222 Power Spectral Density Analysis of V/STOL Aircraft Structures by Melvin J. Rich, Martin H. Israel, Irwin J. Kenigsberg & Peter P. Cook Sikorsky

May 8-10 1968

24 SAE 650193 Helicopters and Propeller-Type VTOL Aircraft in the Light of technologies by W.Z. Stepniewski & M.I. Young Boeing-Vertol

Apr 12-16 1965

25 SAE 660316 The Effect of Size on the Economics of a V/STOL Transport Airplane by George D. Ray Boeing

Apr 25-28 1966

26 SAE 680330 Large Military Transport (V/STOL) by John C. Ford North American Rockwell

Apr 29-May 2 1968

27 SAE 680699 Forward Area Air Cargo Systems by Lewis G. Knapp Sikorsky

Oct 7-11 1968

28 SAE 680301 Possible Navy Applications of V/STOL Transports by Hugo G. Sheridan

Apr 29-May 2 1968

29 The Aerodynamic Effects of Lift Jet and Lift Fan Inlets in Transition Flight by William E. Grahame Northrop

Jun 13 1968

181

30 VTOL Advances as Determined from Analysis of Future Needs and Technological Potentials by Bernard Lindenbaum, Robert Malbi & Richard Krabel AFSC (3 copies)

Dec 6 1967

31 Design Philosophy of Subsonic Compound Aircraft vs. Operational Requirements by W.Z. Stepniewski, J.J. Schneider Boeing-Vertol

Undated

32 Report NO. NA-68-224 Large Military Transport (V/STOL) by John C. Ford NAA/ Rockwell

C.A. 1968

33 Engineering Paper No. 1224 Factors Involved in the Design of a VTOL Propulsion System by Charles O. Gunderson Douglas

Oct 12 1961

34 Application of Optimization Techniques to the Design and Operation of V/STOL Aircraft by W.Z. Stepniewski Boeing-Vertol & M.Z.v.Kryzwoblocki Michigan State Univ.

Apr 3-6 1967

35 Vertical Takeoff Aircraft by L. Gil’berg Oct 26 1960 36 VTOL-STOL Survey for NACA by Grover Loening Nov 30 1957 37 AIAA Paper No. 69-326 Future Military Applications of

VTOL Aircraft by Col. John W. Oswalt & Gen. Hamilton H. Howze

Feb 17-19 1969

38 AHS 13th Annual Forum Military Aspects of VTOL Aircraft Development by LTC John L. Klingenhagen

May 9 1957

39 NASA TN D-735 Handling Qualities Experience with Several VTOL Research Aircraft

Mar 1961

40 Proprotor Short-Haul Aircraft – STOL and VTOL by Kenneth W. Sambell Bell

Jul 5 1972

41 Running Takeoff Overload Limitations of Some VTOL Aircraft Piasecki

May 25 1961

42 Advanced Configurations Boeing Jun 1963 43 Report No. 30863 V/STOL in a 10-Ton Payload Assault

Transport Douglas Apr 27 1962

44 SR-175 3-5 Ton Class Doak Undated 45 Current Status of VTOL Research and Development at

Sikorsky Dec 8 1959

46 V/STOL Capabilities Lockheed-California Undated 47 Vertol Status Report on VTOL Projects 1959 48 VTOL Studies Presentation Chance-Vought Undated 49 Report No. 2-59-945001 Summary of VTOL at Bell

Volume I Nov 1959

50 Report No. G-10-1 V/STOL Concepts Summary Dec 1 1959 51 VTOL Miscellaneous Papers Various 52 VTOL Miscellaneous Photos & Transparencies Undated

STOL/VSTOL PROPOSALS AND CONCEPTS 93 1 YC-14 Brochure Boeing Sep 1976

182

2 YC-15 Brochure McDonnell-Douglas Sep 1977 3 SAE 700811 Synthesis of Future High Lift Systems by

Richard Scherrer Lockheed-California Oct 5-9 1970

4 A Boeing View of Commercial STOL by Richard D. FitzSimmons Boeing

Sep 1969

5 YC-14 AMST Brochure Undated 6 Report No. ER-9801 A Preliminary Report of the

Spanwise Blowing Concept Lockheed-Georgia Mar 1968

7 NASA TN D-2231 A Flight Investigation of the Performance, Handling Qualities, and Operational Characteristics of a Deflected Slipstream STOL Transport Airplane Having Four Interconnected Propellers

Mar 1964

8 Report No. 2-53310/6R-6084 Analysis Report for the C­142 Configuration Study Wind Tunnel Tests Contract# AF 33(657)-16202 LTV

Aug 9 1966

9 Report No. R221-004 Design Studies of High-Speed-Ratio STOL Aircraft Power Plant and Propeller Data Fairchild

Jun 29 1956

10 XC-142 Reviews Aug-Sep 1963 11 Report No. AER-E1R-13339 VHR-447 VTOL Tri-Service

Transport Vol. 1 Detail Specification Hiller, Vought, Ryan Apr 1961

12 Report No. AER-E1R-13342 VHR-447 VTOL Tri-Service Transport Vol. 4 Part 1 Stability and Control Hiller, Vought, Ryan

Apr 1961

13 Report No. AER-E1R-13352 VHR-447 VTOL Tri-Service Transport Vol. 11 Hydraulic System Hiller, Vought, Ryan

Apr 1961

14 Report No. AER-E1R-13354 VHR-447 VTOL Tri-Service Transport Vol. 13 Demonstration Program Report Hiller, Vought, Ryan

Apr 1961

15 A Review of the Structural Dynamic Characteristics of the XC-142A Aircraft by A.L. Head, Jr. Chance Vought

Jun 26-27 1963

16 Dynamic Model Testing of the XC-142 Aircraft by A.L. Head, Jr & W.D. Smith LTV

Sep 23-25 1963

17 Report No. 2-53310/4R939 Estimated Flying Qualities of the XC-142A V/STOL Assault Transport Contract# AF 33(657)-7868 LTV

May 22 1964

18 Report No. 2-53330/9R-6146 Evaluation of Propeller Forces and Moments at High Inflow Angles Including the Effects of Monocycle Action Contract# AF 33(657)-7968 LTV

Sep 19 1969

19 XC-142 VTOL Transport No. 23 Monthly Progress Report Contract# AF 33(657)-7868 LTV

Nov 1963

20 XC-142A System 478A System Package Program Mar 15 1965 21 Report No. 2-55120/2R789 XC-142 Growth Airplane

Payload and Cargo Compartment Size Study LTV May 1962

183

22 Report No. R-221-002A Interim Report No. 1 Design Studies of High-Speed-Ratio STOL Aircraft Contract# Nonr-1733(00)

Jul 29 1955

23 Report No. R-221-002C Interim Report No. 3 Design Studies of High-Speed-Ratio STOL Aircraft Contract# Nonr-1733(00)

Sep 30 1955

24 Report No. R-221-002H Interim Report No. 8 Design Studies of High-Speed-Ratio STOL Aircraft Contract# Nonr-1733(00)

Feb 29 1956

25 Report No. R221-010 Study of STOL Airplane with Direct-Lifting Turbojets M-221G Fairchild

May 31 1965

26 Report No. R221-003 Methods of STOL Airplane Analysis M-221G Fairchild

Jun 21 1956

27 Report No. R224B-005 M224B Vectored Slipstream Tests Contract# DA 44-177-TC-350 Fairchild

Nov 19 1956

28 Report No. R224-006 Interim Summary Report M-224B Contract# DA 44-177-TC-350 Fairchild

Dec 19 1956

29 Report No. R246-001 Jet Wing Configuration Studies Fairchild

Oct 28 1957

30 Short Take-Off and Landing for the High-Speed Aircraft by John K. Wimpress Boeing

Feb 1966

31 IRAD Review Aerodynamics of STOL Lift Systems May 1972 32 XC-142 Material Various 33 SAE 680645 Distributed Suctiion Boundary Layer Control

for High Lift by S.C. Roberts Miss. State Univ. Oct 7-11 1968

34 SAE 710464 The Future of STOL by Richard D. FitzSimmons & LTC William E. Thurman NASA

May 10-13 1971

35 SAE 710465 Comparison of STOL Design Criteria for Commercial and Military Transport Aircraft by Jesse C. Peaslee Boeing

May 10-13 1971

36 SAE 710468 Military/Commercial STOL Transport Commonality by Harold F. Kleckner McDonnell Douglas

May 10-13 1971

37 SAE 710469 STOL Engine Systems and Sensitivity Factors by Joel Godston Pratt & Whitney

May 10-13 1971

38 Synthesis of Future High Lift systems by Richard Scherrer Lockheed-California

Undated

39 AIAA No. 67-741 The Augmentor-Wing Research Program – Past, Present and Future by D.C. Whittley De Havilland Aircract, Canada

Oct 18-200 1967

40 ICAS Paper No. 68-07 Researches About the Use of STOL Aircraft in Civil Transport Aviation. Some Experimental Results on a STOL Aircraft Model by A. Salvetti Univ. of Pisa, IT.

Sep 9-13 1968

41 Aero Report 894 Preliminary Wind-Tunnel Investigation of a Method of Suppressing the Leading-Edge Stall on a Wing by Tangential Blowing by H.R. Chaplin

Mar 1956

184

42 NASA TN D-1857 Large-Scale Wind-Tunnel Tests of Descent Performance of an Airplane Model with a Tilt Wing and Differential Propeller Thrust

Sep 1964

43 NASA TN D-7034 Wind-Tunnel Investigation of a Four-Engine Externally Blowing Jet-Flap STOL Airplane Model

Dec 1970

44 NASA TN D-658 Ground Influence on a Model Airfoil with a Jet-Augmented Flap as Determined by Two Techniques

Feb 1961

45 FTD-MT-24-1674-71 Investigation of the Takeoff-Landing Characteristics of Short takeoff and Landing (STOL) Jet Aircraft by V.I. Surus

May 19 1972

46 USAAVLABS TR No. 68-19 Investigation of the Lateral/Directional Stability Characteristics of a Four-Propeller Tilt-Wing VTOL Model Contract# DA 44-177­AMC-8(T)

Apr 1968

47 Report No. GD/C-64-063A STOL Technology Development and Systems Study General Dynamics/Convair

May 1974

DUCTED/SHROUDED PROPELLER & DOAK, DOUGLAS, HILLER PROPOSALS

94 1 Report No. GDC PIN 66-947 A Proposal for (AID) Addressed Infantry Delivery System Volume I – Advanced Development Technical Proposal General Dynamics

Nov 1966

2 NASA TN D-776 A Wind Tunnel Investigation of a 4­Foot-Diameter Ducted Fan Mounted on the Tip of a Semispan Wing

Feb 1961

3 NASA TN D-981 Aerodynamic Characteristics of a Powered Semispan Tilting-Shrouded-Prepeller VTOL Model in Hovering and Transition Flight

Jan 1962

4 NASA TN D-1301 Aerodynamic Characteristics of a 4­Foot-Diameter Ducted Fan Mounted on the Tip of a Semispan Wing

Apr 1962

5 NASA TN D-1491 Transition and Hovering Flight Characteristics of a Tilt-Duct VTOL Research Aircraft

Nov 1962

6 NASA TN D-1802 Flight Operating Problems and Aerodynamic and Performance Characteristics of a Fixed-Wing, Tilt-Duct, VTOL Research Aircraft

Jul 1963

7 SR-175 3-5 Ton Class VTOL Aircraft Doak 1965-1970 Time Period

Undated

8 Report No. ES 29793 V/STOL Design Studies Douglas Mar 11 1960 9 Report No. ES 29530 VTOL Propulsion System Study

Douglas Sep 25 1959

10 Report No. ES 29735 Preliminary Results of an Analytical Study of Shrouded Propeller Inlet Design Requirements Douglas

Jul 8 1960

185

11 Report No. ES 29674 Model D-793 US Army Surveillance Aircraft Study ASR 2-60 Douglas

Jan 25 1960

12 Report No. ES 29675 Model D-791 VTOL/STOL Tactical Transport Aircraft for the US Army ASR 3-60 Douglas

Jan 25 1960

13 Report No. ES 29759 V/STOL Logistics Aircraft Study SR-175 Vol. I Technical Analysis Douglas

Jan 26 1960

14 Report No. ES 29759 V/STOL Logistics Aircraft Study SR-175 Vol. II Operational Analysis Douglas

Jan 26 1960

15 Report No. ES 40371 Operational Improvement Modification for Army DOAK VZ-4DA Aircraft Douglas

Jun 5 1961

16 Encl. (1) to B-25-M-870 Small Parasite VTOL Aircraft Capabilities

Undated

17 Report No. 680.2 Truck Test Stand Tests of Hiller Airborne Personnel Platform Phase II Hiller

Sep 15 1955

18 Report No. 56-108 Aerodynamics of Ducted Propellers as Applied to the Platform Principle Model No. 1031-A Hiller

Nov 30 1956

19 Report No. ARD No. 111 Some Remarks on the Control and Stability Characteristics of the Flying Platform Hiller

Apr 26 1956

20 Report No. ARD No. 112 Stability Analysis of Flying Platform in Hovering and Forward Flight Hiller

Oct 12 1956

21 Report No. ARD No. 198.1 Proposal for Static Tests of a Ducted Propeller Slipstream Deflection System Hiller

May 17 1958

22 Report No. ARD-233 Dynamic Stability Analysis of Ducted Fan Type Flying Platforms Contract# NONR 1357(00) Phase IV Hiller

May 29 1959

23 Report No. 56-110 Summary Report – Phase III – Airborne Personnel Platform Contract# Nonr 1357(00)

Nov 30 1956

24 Report No. FTD-HT-66-273 Applications of Ducted-Fan Propellers in the Ground Forces by J. Soulez-Lariviere (from French)

Oct 14 1966

25 NORD Cadet 500 Information 1967-1969 26 Piasecki PA-2 Blueprints 1955 27 AERO Report No. 935 Wind Tunnel Tests of a ¼-Scale

Model PA-2C VTOL Aircraft Part I – Power Off Tests Feb 1958

28 AERO Report No. 935 Wind Tunnel Tests of a ¼-Scale Model PA-2C VTOL Aircraft Part II – Tee-Tail Tests

May 1958

29 AERO Report No. 935 Wind Tunnel Tests of a ¼-Scale Model PA-2C VTOL Aircraft Part III – Propulsion System calibration

Mar 1960

30 AERO Report No. 935 Wind Tunnel Tests of a ¼-Scale Model PA-2C VTOL Aircraft Part IV – Power Tests of a VTOL Configuration

Mar 1960

186

DEFLECTED SLIPSTREAM V/STOL 95 1 Report No. 407 The Static and Dynamic Stability of a

Deflected Slipstream Vehicle by G.A. Cincotta & H.S. Dunn Princeton Univ.

Mar 1958

2 Report No. 437 An Investigation of the Fundamental Parameters Which Govern the Aerodynamics of Various Wing-Propeller Combinations as Related to Vectored Slipstream Aircraft by Norman R. Augustine Princeton Univ.

Oct 1958

3 Report No. LR 11908 Aerodynamics CL-346 Dispersed Site VTOL Fighter-Bomber Design Study Contract# AF 18(600)-1642 Lockheed-California

Dec 5 1956

4 Report No. 13063 VTOL-STOL Test Bed Research Aircraft Summary Report Lockheed-California

May 22 1958

5 Report No. 13064 VTOL-STOL Test Bed Research Aircraft Aerodynamics Report Lockheed-California

May 22 1958

6 Report No. 8820-3 Static Characteristics of the Ryan Model 88 Monoplane and Biplane-Type Apparatus for Deflecting a Propeller Slipstream Through Large Angles Contract# NOnr-1710(00) Ryan

Apr 27 1956

7 Report No. 8818-4 TR – Parametric Studies Pertaining to Direct Ascent Aircraft Employing the Deflected Slipstream Principle Contract# NOnr-1710(00) Ryan

Apr 15 1956

8 Report No. 8818-3 Summary Report – Direct Ascent Aircraft Employing the Deflected Slipstream Principle Contract# NOnr-1710(00) Ryan

Apr 15 1956

9 Report No. 709 Report on Wind Tunnel Tests of a 0.20 Scale Model of the DOAK Model 16 Airplane Cal. Institute of Technology

Jan 2 1959

10 Report No. PDR-674A-2 Advanced Shipbased/Dispersed-Site VTOL System (Nutcracker) Grumman

May 1975

11 NASA CR-152132 Study of Aerodynamic Technology for VTOL Fighter/Attack Aircraft Phase I Final Report Contract# NAS2-9772 BY LTV

May 1978

12 Deflected Slipstream Aircraft Photos and Articles Various 13 NASA TN D-649 Loads Induced on a Flat-Plate Wing by

an Airjet Exhausted Perpendicularly Through the Wing and Normal to a Free-Stream Flow of Mach Number 2.0

Mar 1961

14 Report No. DS 210.3 Wind Tunnel report DOAK Model 18 Contract# DA-44-177-TC-351 Doak

Aug 1 1958

15 Dornier Do231 VSTOL Transport Brochure (in German) Undated 16 Report No. DS 210.1 Design, Fabrication, and general

Aerodynamics report of the DOAK Model 16 20% Scale Low-Speed Wind Tunnel Model Contract# DA-44-177­TC-351 Doak

Dec 6 1957

187

17 Report No. DS-208 Revision A Control System Report Contract# DA-44-177-TC-351 Doak

Jul 31 1959

18 Phase II 50 Hour Ground Test Report Doak Model 16 Jul 31 1959 19 Proposal 50-Hour Pre-Flight Ground test Doak Model 16

VTOL Flight Test Vehicle Undated

20 Propulsive Wing Articles, Photos and Brochures Various 21 AHS 24th Annual Forum No. 203 A Promising Concept for

the Joint Development of Military Intra-Theater and Commercial Inter-Urban VTOL Transports by T. Gardner Hill Lockheed-Georgia

May 8-10 1968

22 Report No. D6-9904 Ground Survivability of Aircraft – II, VTOL Dispersal – Survival Boeing

Dec 26 1963

23 AFFDL-TR-70-88 Background Information and User Guide for MIL-F-83300 – Flying Qualities of Piloted V/STOL Aircraft

Nov 1971

VTOL, DOWNWASH 96 1 Report No. LR 20468 Downwash Effects Study Contract#

F33657-67-C-0703 Lockheed-California C.A. 1962

2 V/STOL Aircraft Downwash Characteristics and Simulated Forest Rescue Test ASD

Sep 1967

3 V/STOL Technology Presentation 1978 4 The Value of Various Technology Advances for Several

V/STOL Configurations by W.B. Peck & A.H. Schoen Boeing-Vertol

Sep 13-15 1978

5 Summary of V/STOL State-of-the-Art Bell Undated 6 Report No. D2-4600 VTOL General Information Boeing Sep 9 1959 7 Report No. 65-978-004 A Review of Technical Literature

on Jet Propelled Vertical Takeoff and Landing Aircraft Bell

Jan 3 1953

8 AHS Dayton Chapter Notes and Vuegraphs May 21 1982 9 Report No. LR 14218 V/STOL Airplanes Lockheed-

California Dec 28 1959

10 Report No. D6-6892 Rapid Site Preparation Presentation Boeing

Feb 1964

11 Journal of the Royal Aeronautical Society Volume 66 Number 614 VTOL and STOL: Simple Solutions to Some of the Operating Problems During Take-off and Landing by J.R.C. Fearon & D.H. Norman Rolls-Royce

Feb 1962

12 Survey of Available Material on Downwash Prediction US Army Material Command

Feb 1971

13 Propulsion/Airframe/Aerodynamics Integration Presentation

Undated

14 V/STOL Aircraft Technology Assessment USAF Flight Dynamics Lab

Oct 1968

188

15 WADD TN 59-374 A Study of Vertical and Short Take-Off Landing Propulsion System State-of –the-Art

Dec 1959

16 Report No. 64575 Assault Transports 1960-1965 Logistics Systems Study ORD 150 Lockheed-Georgia

May 30 1958

17 Material from By Winborn Early VTOL Various 18 Report No. DR-1744 Level Attitude, Propellered VTOL

Comparative Study USNavy BuAir Mar 1957

19 NASA TN D-733 Review of Basic Principles of V/STOL Aerodynamics

Mar 1961

20 Rotor Recovery Systems Various 21 V/STOL Aircraft Designs Article for AAHS plus

Supporting Documents Undated

22 SAB Briefing Papers 1967 23 WADC TR58-564 Appendix I Bibliography of Report

References C.A. 1958

24 Report Bibliography – Tail-Sitter Aircraft May 31 1972 25 Report No. PAR 238/10 Report of Ad Hoc Group on Short

and vertical Take-Off and Landing Aircraft Nov 15 1956

26 Design Considerations for VTO Aircraft Hiller Undated 27 Book on Vertical Flight In German Jan 1961 28 Miscellaneous Articles and Papers on Vertical Flight Various

TILT-WING, X-18(HILLER MODEL 1051), GEM, STOPPED-ROTOR COMPOUND HELO

97 1 X-18 Correspondence Hiller 1960-1961 2 X-18 Blueprints Hiller Sep 1956 3 X-18 Inspection Report Oct 27-28 1959 4 Report No. 461.3 A Simplified Theoretical Investigation of

a Wing-Propeller Combination Through a Range of Angle­of-Attack from 0o to 90o and a Comparison with Experimental Results Hiller

Oct 15 1955

5 Report No. 56-65 The Aerodynamic Characteristics of Tilt-Wing Propelloplane Model 1051 Hiller

Jul 17 1956

6 Report No. 56-79 Specification for Ground testing of the X-18 Tilt-Wing, VTOL, Test Bed Contract# AF 33(600)­32749 Hiller

Sep 14 1956

7 Report No. 56-68 Wind Tunnel Test Program for Model 1051 Tilt-Wing Flying Test Bed Hiller

Aug 7, 1956

8 Report No. 56-78 Specification for Flight Testing of the X­18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)­32749 Hiller

Sep 14 1956

9 Report No. 56-97 Preliminary Design Study Summary Report – Tilt-Wing, VTOL, Test Bed, X-18 Contract# AF 33(600)-32749 Hiller

Oct 11 1956

189

10 Report No. 57-58-1 Estimated Flight Test Performance – X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)­32749 Hiller

May 31 1957

11 Report No. 57-58-2 Estimated Flight Test Performance – X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)­32749 Hiller

May 31 1957

12 Report No. 57-114-3 Ground and Lift-Off Test Schedule for the X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller

Oct 7 1957

13 Report No. 58-74 An Analysis of the Variation of Pitching Moment in Transition Flight – X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller

May 27 1958

14 Report No. 58-80 Flight Test Schedule for the X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller

Nov 1 1958

15 Report No. 58-130 Force Testing of a One-Eighth Scale Model X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller

Oct 6 1958

16 Report No. 58-132 Available Thrust Analysis – J34-WE­36 Pitch Control Engine Installation X-18 Aircraft Hiller

Oct 28 1958

17 Report No. 58-136 Remote-Controlled Free-Flight Test of a 1/8-Scale Model X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller

Oct 31 1958

18 Report No. 58-154 Estimated Performance Report X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller

Dec 1 1958

19 Report No. 59-15 Flight Simulation of the X-18 in Hover – Edwards AFB Contract# AF 33(600)-32749 Hiller

Feb 4 1959

20 Report No. 59-34 Airplane Stability and Control – X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller

May 15 1959

21 Weight and Balance Status Report No. 37 X-18 Tilt-Wing VTOL Test Bed Contract# AF 33(600)-32749 Hiller

Nov 15 1959

22 Report No. HTC 64-38 Interim Report Rotor-Wing Concept Study Contract# Nonr-4588(00) HTC

Oct 1964

23 Report No. 859-099-001 Trailing Rotor Convertiplane Model Rotor System Wind Tunnel Test Contract BHC W.O. 4280-059; R.T. 059-1 Bell

Aug 14 1964

24 Report No. 5059-099-001 Trailing Rotor Convertiplane Configuration Study Twin Rotor TRC-1A Contract# BHC WO 5059; RT 059-1 Bell

Feb 10 1965

25 Report No. SEP-6260 Stowed Rotor V/STOL Proposal Sikorsky

Oct 30 1964

26 Report No. LR 17844 Proposal for a Stopped Rotor Research Compound Helicopter Lockheed-California

May 7 1964 Rev Jun 3 1964 Rev Aug 10 1964

190

27 Proposed Program for R&D Hot Cycle Rotor-Wing High Speed VTOL Aircraft Concept Hughes

Undated

28 Report No. 2017-933001 GEM Morphology Study Progress Report Contract# Nonr-3074(00) Bell

Nov 14 1960

29 Report No. ZP-319 Study of Impact Loads and Motions of Ground Effect Machines (GEM) Report to Contractors Meeting Convair

Nov 16-18 1960

30 Report No. AP-5024-R Third Progress Report GEM Propulsion System Study Contract# Nonr 3024 Garrett

Nov 11 1960

31 Letter 65T-0209/2189 Progress Report No. 1 Rotor/Wing Wind Tunnel Tests at David Taylor Model Basin: Stopped Rotor Tests Contract# Nonr 4588(00) HTC

Apr 7 1965

32 Progress Report No. 2 Rotor/Wing Wind Tunnel Tests at David Taylor Model Basin: Stopped Rotor Tests HTC

May 26 1965

33 Alouette 3 Brochure SUD Jan 1960 34 SA. 3210 Brochure SUD Feb 1960 35 Alouette II Brochure SUD Undated 36 Djinn IIIB Brochure SUD Jan 1960 37 Djinn Description Brochure SUD Undated 38 Fiat 7005 Helicopter Brochure Fiat Oct 1964 39 Fiat 7005 Photos Fiat C.A. 1964 40 Fiat 7002 Blueprints 1958 41 Lindenbaum File – Assorted Photos and Sketches Undated

VECTORED THRUST & DIVERTED SLIPSTREAM VTOL

98 1 NACA TN 3919 Investigation of Effectiveness of a Wing Equipped with a 50-Percent-Chord Sliding Flap, a 30­Percent-Chord Slotted Flap, and a 30-Percent-Chord Slat in Deflecting Propeller Slipstreams Downward for Vertical takeoff

Jan 1957

2 NASA TN D-89 Wind-Tunnel and Piloted Flight Simulator Investigation of a Deflected-Slipstream VTOL Airplane, The Ryan VZ-3RY

Nov 1959

3 NASA TN D-331 An Examination of Handling Qualities Criteria for V/STOL Aircraft

Jul 1960

4 NASA TN D-433 Low-Speed Measurements of Static and Oscillatory Lateral Stability Derivatives of a 1/5-Scale Model of a Jet-Powered Vertical-Attitude VTOL Research Airplane

Sep 1960

5 NASA TN D-735 Handling Qualities Experience with Several VTOL Research Aircraft

Mar 1961

6 Report No. N79-10024 Study of Aerodynamic Technology for VSTOL Fighter/Attack Aircraft – Horizontal Attitude Concept Northrop

May 1978

191

7 Report No. FTC-TR-66-30 Flight Evaluation of the XV-5A VSTOL Aircraft

Mar 1967

8 Report No. 407 Dynamic Stability Analysis of a VTOL Vectored Slipstream Vehicle During Transition by Guy G. Williamson Princeton Univ.

Mar 1958

9 Report No. 535 The Static and Dynamic Stability of a Deflected Slipstream Vehicle by G.A. Cincotta & H.S. Dunn Princeton Univ.

Apr 1961

10 Report No. UER 18-601 Maintenance and Rigging Manual for Air & Space Model 18A Gyroplane Air & Space

Mar 30 1965

11 Report No. TS 3080 An Evaluation of the Harrier AV-8A and the Pegasus Engine Rolls-Royce/British Aerospace

Dec 1978

12 Recent Ejector Technology Programs at the Naval Air development Center by K.A. Green

C.A. 1979

13 Status and Trends in Powered Lift Systems by Peter G. Kappus

Undated

14 A Simple Graphical Method for Evaluating the Effect of Thrust Vector Tilt on the Aircraft Performance by Peter Bielkowicz

Jul 1 1968

15 The Rebirth of the Tiltrotor by Robert R. Lynn Bell Jun 1992 16 Vectored Thrust – Europe Photos & Graphs Various 17 Vectored Thrust – Dassault(Fr) Photos Various 18 Vectored Thrust - Hawker-Sidderly (UK) Photos &

Articles Various

19 Vectored Thrust – Fiat(It) Photos Various 20 Vectored Thrust – VFW(Ge) Photos & Articles Various 21 Vectored Thrust – VFW VAK-191B Photos & Articles Various 22 Vectored Thrust – Hawker-Sidderly KESTREL P-1127

Photos & Articles Various

23 Vectored Thrust US/FRG Fighter Photos Various 24 Vectored Thrust – Short SC.1 Photos Various 25 Vectored Thrust – Dassault(Fr) MIRAGE III Photos Various 26 Vectored Thrust – Bell D-188A Article Undated 27 Vertical Thrust – Boeing Tri-Service Transport Various 28 Vertical Thrust – USSR Various 29 Vertical Thrust – Northrup Various 30 Vertical Thrust – SUD/EWR Various 31 Vertical Thrust – Vought Various 32 Vertical Thrust - Hiller/Vought/Ryan XC-142A Various 33 Custer Channel Wing (CCW) Concept and Information 1971 34 Roadable Aircraft Various 35 Individual Mobility Concepts Various 36 Lift-Fan Material Various 37 Report No. 2-60-953001 V/STOL Fighter-Bomber State­

of-the-Art Presentation Bell Oct 1960

38 WASP II – Preliminary Airworthiness Evaluation Jun 1982

192

39 Foreign V/STOL Progress 1965 40 Turbo-Jet/Turbo-Fan MVTOL Technology Status NAA Nov 1965 41 Turbulence Measurements in an Ejector Wing Flow Field

by G.D. Catalano – LSU, H.E. Wright & D. Stevens – AFIT, K.S. Nagaraja – AF Wright Labs

Aug 3-5 1981

42 AIAA Paper No. 71-980 The V/STOL Projects of the Federal Republic of Germany by Drury W. Wood Dornier

Oct 25-28 1971

43 SAE No. 680644 Low-Speed Characteristics of High-Performance Lift-Engine V/STOL Aircraft by Jerry P. Barrack & Jerry V. Kirk NASA Ames

Oct 7-11 1968

44 Kestrel P-1127 Evaluation Trials by Major John A. Johnston USA

Undated

45 Studies of the Transition of VTOL-Aircraft by S. Gunter Undated 46 ICAS Paper No. 68-49 Developing a V/STOL Combat

Aircraft by B.P. Laight Hawker-Sidderly Sep 9-13 1968

47 AHS Paper No. 234 Experience of and Methods to be Used in Clearing a Jet-Lift Aircraft for Service Use by Ian A. Fisher

May 8-10 1968

48 AHS Paper No. 220 Control Characteristics of Vectored Thrust V/STOL Vehicles in the Transition Regime by Alan V. Coles Bell

May 8-10 1968

49 IAS Paper No. 624 Reverse Thrust, Vertical Lift, and Side Force by Means of Controlled Jet Deflection by Leonard Meterhoff – Brooklyn Polythecnic & Stanley Meterhoff – Eastern Research Group

Jan 23-26 1956

50 AIAA Paper No. 78-1082 Aerodynamic Effects Induced by a Vectored High Aspect Ratio Nonaxisymmetric Exhaust Nozzle by Douglas L. Bowers AF Flight Dynamics Lab

Jul 25-27 1978

51 AIAA Paper No. 78-956 Design and Experimental Studies of a Type A V/STOL Inlet by H.C. Potonides, R.A. Cea & T.F. Nelson Grumman

Jul 25-27 1978

52 AIAA Paper No. 78-1022 Installed Performance of Vectoring/Reversing Nonaxisymmetric Nozzles by P.E. Hiley, D.E. Kitzmiller & C.M. Willard McDonnell Douglas

Jul 25-27 1978

53 Miscellaneous VTOL Photos & Articles Various 54 Report No. 62B125 XV-5A Detail Aircraft Specifications

Contract# DA44-177-TC-715 Ryan Dec 15 1962

55 Report No. 477 A Stability Analysis of Tilt-Wing Aircraft (Analytical) by Charles H. Cromwell III & Henry E. Payne III Princeton Univ.

May 1960

56 Report No. 478 A Stability Analysis of Tilt-Wing Aircraft (Experimental) by Charles H. Cromwell III & Henry E. Payne III Princeton Univ.

May 1960

193

SERIES IX: Escape Systems, Crash and Rescue, 1929-1999

Box File Description Date

ESCAPE SYSTEMS 99 1 Report R-760 Technical Proposal for Stowable Aircrew

Vehicle Escape Rotoseat AERCAB Concept Volume I Kaman

Oct 11 1968

2 Report PDR-306-1 Grumman Project 306 Surface to Air Retrieval of Heavy Spacecraft by Fixed-Wing Aircraft Contract# NAS9-195

Jun 1962

3 Report P-3003 Interim Progress Report IPR-4 SR-49759 Retrieval Concept Study

Feb 28 1961

4 Saver AERCAB Test Data & Results Briefing Notes C.A. 1970 5 Discretionary Descent Using Rotary Wings by B.

Lindenbaum Undated

6 AERCAB Phase III Program Review Fairchild-Hiller Mar 2 1971 7 Proposal (09-0198) for the Development of a Prototype

Aircraft Escape System Parsons Corp. Apr 21 1969

8 Report GAP-68-5189 Integrated Aircrew Escape/Rescue System Capability (AERCAB) Goodyear

Oct 10 1968

9 Report GER 8597 Summary ER on the Development of a Two Place Inflatoplane Contract NOnr 1860(00)

Jul 31 1958

10 Goodyear Inflatoplane Brochures 1971 11 Report No. 15-94-1 Report on Performance Tests of

Rotochute Models Contract# W33-038 ac-18190 Oct 8 1948

12 Report No. 15-130-1 Basic ER Rotochute Phase I Contract# W33-038 ac-18190

Nov 9 1948

13 Report No. 55230 Development of “Rotochute” Rotary Wing Air Brake GE

Nov 3 1947

14 Report TSEAL2-672-1-2 Flight Tests of the Gyro-Container

Mar 30 1945

15 Proposal 520/35-4/RL Development of the Helicycle Vehicle Revision A Wyle Labs

Jun 7 1958

16 NACA RM L54B12a Flight Tests of a Man Standing on a Platform Supported by a Teetering Rotor

Mar 24 1954

17 Mobility Effectiveness of Air Cushion Craft by William C. Walter

Undated

18 NASA TN D-189 Static-Stability of a Stand-On Type Helicopter with Rigid Blades, Including a Comparison of Theory

Feb 1960

19 Discretionary Descent – Clippings and Information Various 20 Discretionary Descent – Project File Various 21 Report No. ARD-233 Dynamic Stability Analysis of

Ducted Fan Type Flying Platforms Contract# NONR 1357 (00) Phase IV

May 29 1959

194

22 AFFDL-TR-66-97 Study of Heavy Equipment Aerial Delivery and Retrieval Techniques

Jan 1967

23 Approaches to Individual Lifting Devices by B. Lindenbaum

Undated

24 Report GER-8465 Proposed Air Rescue System (Mother-Daughter Concept) Goodyear

Dec 18 1957

25 NACA RM L52D10 Preliminary Experimental Investigation of the Flight of a Person Supported by a Jet Thrust Device Attached to His Feet

Jan 15 1953

26 AHS Newsletter Vol. 2 No. 12 Dec 1956 27 Report No. 404 Stability and Control of Unducted Stand-

On Helicopters: Preliminary Theoretical and Flight Test Results Contract# DA 44-177-TC-392 Princeton Univ.

Nov 1957

28 Report TR-737 Jet Lift Concepts to Improve Individual Soldier Mobility Thiokol

Jun 3 1959

29 Report TR 3355-1 Rocket Jump Belt Thiokol Aug 1 1960 30 Introducing the Reaction Motors – Rocket Jump Belt

Thiokol Undated

31 Jump Belt Photos and Articles Various 32 Report ARD-236 Summary Report Airborne Personnel

Platform Contract# Nonr 1357(00) Jun 9 1959

LOCAL CRASH RESCUE HELICOPTERS 100 1 Report AU-74b Model Specification XR-9B Helicopter

G&A Aircraft Jul 4 1945

2 FSTC-HT-23-911-72 Results of the Theory of Rotor Flow According to Miller and Scully (W. German)

Aug 23 1972

2 YH-41 (Modified) Air Force Local Crash Rescue Helicopter Cessna

Undated

3 The Piasecki Story of Vertical Flight Brochure C.A. 1969 4 AF TR No. 6162 Development of the G&A Model XH-9,

XH-9A, and XH-9B Helicopters May 1950

5 Report No. 47-945-045 Model 47J Local Crash Rescue Mission – Weight and Balance

Jul 20 1956

6 Hughes OH-6A Physical Configuration and Flight Characteristics

Undated

7 AF TR No. 6272 Performance Testing Methods for Helicopters

Dec 1950

8 Report No. 57-76 Two-Place Observation Helicopter Preliminary Design Study Hiller

Aug 1957

9 Report HTC-AD 64-25 Design Specification – Hughes 300 Model 269B Helicopter

Undated

10 Report No. SER-100 Stress Analysis of Main Rotor Head Contract# W535 AC-29845 DA W535 AC 2514 Sikorsky

Aug 1 1943

195

11 Report No. X-1513 Flight Test Report XR-4B Section III – Synchronization of the Throttle with the Main Pitch Control Contract W535 AC-29845 Change 1 DA W535 AC 2514

Aug 27 1943

12 AFFTC 52-41 Phase IV Performance Tests of the H-23B Helicopter

Dec 22 1952

13 DAVI – Dynamic Antiresonant Vibration Isolator Kaman Undated 14 Development of the Helicopter Lockheed Dec 1967 15 Progress in Rotor-Blade Aerodynamics by P.F. Yaggi &

I.C. Statler USAAMRDL C.A. 1971

16 AFFTC-TR-57-12 H-13H Phase IV Performance Test Jul 1957 17 AFFTC-TR-57-12 H-13Addendum no. 1 Phase IV

Performance Mar 1958

18 FSTC-HT-1348-71 Specifics of Aerodynamics of the Lifting Rotor of a Helicopter by A.M. Mkhitaryan (USSR)

1970

19 YH-41 (Modified) Air Force Local Crash Rescue helicopter Preliminary Model Specification Cessna

Jul 30 1956

20 YH-41 (Modified) Air Force Local Crash Rescue Helicopter Performance Report Cessna

Jul 30 1956

21 Report HTC-AD 369-Y-8003 Detail Specification for a Single Engine, Single Main Rotor Light Observation Helicopter Army Model Designation OH-6A Contract IFB AMC(T)23-204-65-222

Apr 21 1965

22 AFFTC-TR-59-33 YH-40 Performance Evaluation Jan 1960 23 AWST Article Hughes269A Aimed at Untapped market Jan 15 1962 24 NACA TN 2154 An Analysis of the Autorotative

Performance of a Helicopter Powered by Rotor-Tip Jet Units

Jul 1950

25 YH-41 (Modified) Air Force Local Crash Rescue Helicopter Weight and Balance Report Cessna

Jul 30 1956

26 YH-41 (Modified) Air Force Local Crash Rescue Helicopter Summary Report of Flight Tests (CH-1A) Cessna

Jul 30 1956

27 Gazelle Brochure Undated 28 Enstrom Guardian II Police/Ambulance Helicopter

Brochure Undated

29 FTD-HC-23-0697-72 Bolkow BO 105 Multipurpose Helicopter (W. German)

Aug 31 1972

30 Optimization of Design Data for Reaction Drive Helicopters by Werner Goller Dornier

Jan 1970

31 Bristol 173 (Hafner) Parts Pictures Undated 32 Doman-Frasier Helicopters – Rotor Head Assembly

Blueprint May 17 1948

33 Design Details of Aeronautical Products, Inc. Helicopter Jun 1945 34 Principles of Helicopter Design (INCOMPLETE) by

Wayne Wiesner Hiller Undated

196

35 NASA TN D-38@ Effect of Blade Cutout on Power Required by Helicopters Operating at High Tip-Speed Ratios

Sep 1960

36 Ground and Flight Test Experience with the Westland Scout Hingeless Rotor Helicopter

Sep 20-23 1971

37 AGARD Advanced Rotorcraft Meeting Notes and Papers Sep 20-23 1971 38 Limitations in Helicopter Design by J.A.J. Bennett Feb 22 1947 39 MC-9 Helicopter Blueprints Mar 5 1952 40 Kaman Model K-190 Utility helicopter Brochure Undated 41 Assorted Helicopter Brochures Undated 42 AHS Assorted Presentations Various 43 Use of Thrust and Lift Augmentation for Increasing

Helicopter Operating Speed by Donald W. Robinson Jr. Kaman

Jan 23 1963

44 What’s Wrong with Today’s helicopters by F.N. Piasecki Jun 20 1950 45 Miscellaneous Articles Various 46 Patent Copies, Helicopter Related

LOCAL CRASH/ RESCUE HELICOPTER & ROTOR AERODYNAMICS

101 1 Report No. DR-210 General Description and Preliminary Model Specification Doman LZ-5-3 Local Crash Rescue Helicopter

Jul 24 1956

2 Report No. DR-211 Preliminary Weight and Balance Report Doman LZ-5-3 Local Crash Rescue Helicopter

Jul 27 1956

3 Report No. DR-212 Preliminary Performance Report Doman LZ-5-3 Local Crash Rescue Helicopter

Jul 27 1956

4 Report No. DR-216 Design, Development, Testing Service, Life and Overhaul Doman LZ-5-3 Local Crash Rescue Helicopter

Jul 30 1956

5 Report No. DR-228 Performance Characteristics of the Doman LZ-5 with the Artouste III or Turmo III French Gas Turbine

Dec 12 1956

6 CAA Approved Rotorcraft Flight Manual for Model LZ-5 Helicopter

Dec 30 1955

7 Drawings and Photographs – Crash Rescue, Uses and Applications, and Design Features Doman LZ-5-3 Local Crash Rescue Helicopter

C.A. 1956

8 USAAVLABS TR 69-94 An Experimental Investigation of the Effects of Rotor Head Configuration and Fuselage Yaw on the Wake Characteristics and Rotor Performance of a 1/8 Scale Helicopter Contract# DA 44-177-AMC-203(T)

Feb 1970

9 State of the Art Advancement in Helicopter Design Lockheed-California

Oct 1963

10 Report No. 204-099-308 Moment of Inertia Calculations – XH-40 Helicopter Contract# AF 33(600) 30229

Dec 19 1956

197

11 Report No. TB-1288-F-1 / WADC TR 59-754, Part I Flight Test Determination of Lateral Stability and Control Derivatives for a Single Rotor Helicopter

Aug 1959

12 Technical Papers – Rotary Wing Pre 1946 13 Report No. 100 Helicopter Blade Analysis Contract# W33­

038 AC5238 Princeton Univ. Jan 31 1947

14 Report No. BB-437-S-1Helicopter Dynamic Stability and Control Studies Part I Contract# W33-038 ac 14248 Exh. J Cornell Univ.

Sep 29 1950

15 Report No. BB-437-S-2 Helicopter Dynamic Stability and Control Studies Part II Contract# W33-038 ac 14248 Exh. J Cornell Univ.

Jun 1 1951

16 An Aerodynamic Comparison of Two Airfoils Based Upon Full Scale Rotor Whirl Tests by Lt. Hamilton R. Harris & Henry R. Velkoff WADC

Sep 1958

17 R. & M. No. 2695 Wind-Tunnel Tests on a 12-ft Diameter Helicopter Rotor

1953

18 Helicopter Blind Flying Trials Fairey Aviation Ltd. Undated 19 WADC TR 55-438 The Determination of Helicopter

Longitudinal Stability Derivatives from Flight Test Data Part II

Mar 1959

20 NACA Wartime Report Airfoil Section Data from Tests of 10 Practical-Construction Sections of helicopter Rotor Blades Submitted by the Sikorsky Aircraft Division, United Aircraft

Sep 1944

21 NACA MR L5C10 Flight Tests of the Sikorsky HNS-1 (Army YR-4B) Helicopter Part I

Mar 1945

22 NACA MR L5D09a Flight Tests of the Sikorsky HNS-1 (Army YR-4B) Helicopter Part II

Mar 1945

23 NACA MR L5C29a Full-Scale-Tunnel Performance Tests of the PV-2 Helicopter Rotor

Apr 1945

24 NACA Restricted Bulletin L5K02 Aerodynamic Characteristics of Four NACA Airfoil sections Designed for Helicopter Rotor Blades

Feb 1946

25 SAE 1999-01-5609 Rotary Wing Flight Display Test and Evaluation by Richard L. Newman Crew Systems

Oct 19-21 1999

26 AIAA 99-3421 The Fluid Dynamics of Rotor Wakes: Theory, Computation and Experiment (Invited) by A.T. Consilk Ohio State Univ.

Jun28-Jul 1 1999

27 Report No. 63B063 Ryan Vertiwing Jul 15 1963 28 Report No. HTC-AD-66-1 TR Hot Cycle Rotor/Wing

Composite research Aircraft Section I Summary of Design HTC

May 1966

29 High Speed VTOL Recovery/Transport Aircraft HTC C.A. 1966 30 Report No. LR 21776 Responses to Questions Regarding

Stoppable Rotor Concepts Lockheed-California Aug 19 1968

198

31 Report No. 67-1 Reverse-Velocity Rotor Program Fairchild-Hiller

Nov 15 1967

32 TCREC TR 62-109 An Experimental Investigation of a Second Harmonic Feathering Device on a UH-1A Helicopter Contract# DA-44-177-TC-806

Jun 1963

33 AHS #603 Design Considerations of Circulation Control Blades by Robert M. Williams & Ernest O. Rogers Naval Ship R&D Center

May 1972

34 R. & M. No. 2997 Second Harmonic Control on the Helicopter Rotor by W. Stewart

Aug 1952

35 NASA TN D-73 Comparison of Calculated and Measured Stall Boundaries of a Helicopter Rotor at Advanced Ratios from 0.3 to 0.4

Sep 1959

36 The Propulsion of Helicopter Rotors by Edward A. Stalker Univ. of Michigan

Undated

37 Helicopter Photos, Articles and Hand Written Calculations C.A. 1949 38 An Introduction to Soviet Helicopters Brown & Shaw

Company Oct 1962

39 R. & M. No. 331, 1132, 1157 Pre 1929 40 NACA RM L51H20a Some Flying-Qualities Studies of a

Tandem Helicopter Oct 1951

41 NACA RM L53F15a Studies of the Speed Stability of a Tandem Helicopter in Forward Flight

Aug 13 1953

42 NACA TN 1799 On the Flying Qualities of Helicopters Jan 1949 43 NACA TN 2309 Charts for Estimation of Longitudinal-

Stability Derivatives for a Helicopter Rotor in Forward Flight

Mar 1951

44 NACA TN 2459 Some Effects of Varying the damping in Pitch and Roll on the Flying Qualities of a Small Single-Rotor Helicopter

Jan 1952

45 NACA TN 3156 Charts for Estimating Tail-Rotor Contribution to Helicopter Directional Stability and Control in Low-Speed Flight

May 1954

46 NACA TN 3201 Directional Stability Characteristics of Two Types of Tandem Helicopter Fuselage Models

May 1954

47 NACA TN 4330 Flow Induced by a Rotor in Power-On Vertical Descent

Jul 1958

48 NASA TN D-97 A Note on the Calculation of Helicopter Performance at High Tip-Speed Ratios

Sep 1959

49 F-TS-688-RE Longitudinal Stability of the Helicopter in Forward Flight by K. Hohenemser (from German)

Aug 1946

50 F-TS-691-RE Lateral Stability of the Helicopter in Forward Flight by K. Hohenemser (from German)

Aug 1946

51 F-TS-692-RE The Pull-Up of the Helicopter by K. Hohenemser (from German)

Aug 1946

199

52 F-TS-1002-RE The Dynamic Stability of Helicopters with Articulated Rotors by Sissingh (from German)

Sep 1946

53 F-TS-1004-RE The Theory for the Control of the Blade Angle of the Helicopter by K. Hohenemser (from German)

Sep 1946

54 F-TS-1005-RE Theory of Oscillations of Blades in the Plane of Rotation by Dr. Kurt Hohenemser (from German)

Sep 1946

55 F-TS-1006-RE Theory of Helicopter Control in Hovering Flight by Dr. Kurt Hohenemser (from German)

Sep 1946

SERIES X: Power Plants, Propellers, RPV, Drone, Small Tactical Aerial Vehicle, and STAMP, 1930-1981

Box File Description Date

RPV/DRONE 102 1 MIL-A-8860(ASG) Military Specification: Airplane

Strength and Rigidity, General Specification for May 18 1960

2 Airplane and Runway Floatation, Document and Pamphlet Boeing

Jul 1979

3 Navy Remotely Piloted Vehicles (RPVS) for Non-Aviation Ships

1976

4 Remotely Piloted Vehicles and Recovery Systems, Pamphlets and Articles

1976

5 Teleplane Briefing Nov 22 1971 6 Rotor Recovery System-Horizontal Type, Notes and

Calculations May 25 1976

7 Balloon Based Recovery System for RPV Notes, Drawings and Calculations

Oct 6 1977

8 VTOL Drone for Army Battlefield Use, Notes and Calculations

1974-1976

9 RPV Correspondence 1976 10 Stoppable Rotor VATOL, Notes and Drawings 1976 11 Para Drone Tasker Systems 12 AFFDL(PTB) TM-71-1 Teleplane Preliminary Design

Study Dec 1971

13 IR&D Project# 0103D8 Summary Report on Low Cost Rigid Structures for Drones Goodyear

Aug 8 1972

14 Drones – XMQM-105 and XBQM-106 Pamphlets 15 Drones for Aerodynamic and Structural Testing (DAST) Aug 1979 16 MQM-107 Overview Pamphlet Undated 17 MQM-107A Overview Pamphlet Undated 18 Mini-RPV Concept Articles 1977 19 RPV Industry Conference: Agenda, Notes, Handouts and

Drawings Feb 23-24 1978

20 NARPV Proceedings and Pamphlets 1976

200

21 High Lift Wing for RPV Recovery: Notes, Graphs and Drawings

Jul 1977

22 DAAB07-78-Q-1533 Mini-RPV Automatic Recovery System Contract Proposal and Notes

Dec 30 1977

23 Ryan Flexbee Surveillance Drone System and Photos Undated 24 RPV Industry Pamphlets Undated 25 Propeller Propulsion for RPV’s: Articles and notes 1976 26 Report R-585-1 The Aeroelastic Behavior of Rotary Wings

in Forward Flight Volume II Correlation with a Servo-Flap Rotor System Contract#64-0488f Kaman

Undated

27 The Application of Reliability Concepts to Fatigue Loaded Helicopter Structures

May 3 1962

28 WADC TR 59-714 Study and Development Criteria for High-Speed Power Transmission Shafts

Dec 1960

29 FTD-TT-63-792 Flexible Heavy-Duty Transmissions Undated 30 Rotor Systems and Control Problems in the Helicopter Sep 5 1947 31 Resonant Fatigue Failures Associated with Noise 32 WCT 2366 Phase II Flight Tests of the Seibel YH-24SE

Helicopter, USAF 51-5113 Oct 22 1951

33 TN WCT-52-47 Functional Development Test of the YH­24SE Helicopter

Dec 1952

34 AFFTC-TH-59-4 Limited Performance Evaluation of the H-43A Helicopter

Mar 1959

35 AFFTC-TR-60-2 Air Force Flight Evaluation of the YHO­2HU Helicopter

Feb 1960

36 Theoretical Investigation of Coaxial Rigidly-Mounted, Two-Bladed Rotors, Final Report Contract# W 33-038 AC-9772 Bendix

Aug 7 1946

37 USAAVLABS TR 70-59 Effect of Rotor Blade Root Cutout on Vertical Drag Contract# DAJ02-70-C-0010

Oct 1970

38 USAAVLABS TR 70-24 An Investigation on the Structural Dynamics of Helicopter Rotors Contract# DAAJ02-67-C-0099

Apr 1970

39 WADC TR 55-437 Part II An Investigation on the Handling Qualities of a Sikorsky H-19 Helicopter Equipped with Various Mechanical Stabilizers Contract# AF 33(616)-2780

Mar 1959

40 Natural Antiresonances in Structural Dynamics Sep 24 1971 41 Application of Advanced Composites to Helicopter

Airframe Structures May 1974

42 The Application of Fracture Mechanics to the Design of Damage-Tolerant Components of the UTTAS Helicopter

May 1974

43 The Use of Test Data to Improve Large Scale Dynamic Models of Structures

Nov 8-9, 1973

44 WADD TR 61-177 Structural Safety Under Conditions of Ultimate Load Failure and Fatigue

Oct 1961

201

45 WADC TR59-507 Fatigue of Aircraft Structures Aug 11-13 1959

POWERPLANTS 103 1 An Experimental Investigation of a Low-Speed

Circulation-Controlled Aerofoil by R.J. Kind & D.J. Maull Cambridge University

Jul 1967

2 Tech Proposal No. 927 Model A51605-274 Propeller for Bell Aircraft Model D190-B Aeroproducts

Jul 1959

3 AHS 24th National Forum – No. 213 The Toroidal Rotary Regenerator for Gas-Turbine Engines by Henry J. Selfors Pratt & Whitney

May 8-10 1968

4 AHS 24th National Forum – No. 212 Allison T63 Regenerative Engine Program by Edward J. Privoznik General Motors

May 8-10 1968

5 LTS 101 Turboshaft Engine Avco Lycoming Apr 1974 6 LTS 101 Turboshaft Engine Avco Lycoming Apr 24 1974 7 T5508D Turbine Engine for the Bell Model 214B Avco

Lycoming Undated

8 USAAVLABS TR 66065 An Experimental Investigation of the Effect of Forward and Rearward Motion on the Thrust of a Shrouded Propeller Contract# DA 44-177­AMC-892(T)

Sep 1966

9 NASA CR-121095 High-Tip-Speed, Low-Loading Transonic Fan Stage – Part I Aerodynamic and Mechanical Design Contract# NAS 3-13498

Apr 1973

10 Proceedings of the 1980 Conference on Propeller Propulsion

Apr 1980

11 Report DM 62-14 A Comparison of VTOL Propulsion Systems in a Subsonic Mission by W.L. Rodenbaugh General Electric

Jan 18 1962

12 High Bypass Turbofan Engines Avco Lycoming Undated 13 Advanced Lift Cruise Engines and Lift Fan Systems Pratt

& Whitney May 17 1966

14 Report PDS-3384 STF/S-351 Convertible Engine Studies 2500-6000 SHP Pratt & Whitney

Sep 5 1969

15 Report GP 73-127RVP Propulsion Summary Pratt & Whitney

Undated

16 USAAVLABS TR 69-59 Detailed Design of a 2000-SHP Advanced Technology V/STOL Propeller System

Sep 1969

17 IAS Paper No. 59-107 Wind Tunnel Tests of Shrouded Propellers and Their Application by Robert K. Wattson, Jr & Vernon O. Hoehne Univ. of Wichita

Jun 16-19 1959

18 FTD-MT-24-141-70 Gas Turbine Engines for Helicopters (from Russian)

Jun 24 1971

202

19 Report HSER 2417 Static Whirl Test Evaluation of a Full-Scale Variable Camber Propeller Phase I Contract# Now 60-0564-d Hamilton Standard

May 31 1961

20 Experimental Rotating Combustion Engines – A New Shape in Power Curtiss

C.A. 1963

21 SAE 650200 Advanced Propeller Developments for V/STOL Aircraft by George Rosen Hamilton Standard

Apr 12-15 1965

22 SAE 730911 Lycoming LTS 101 – Low Cost Turbine Power in the 600 hp Class by A. Myers & E. Pease Avco Lycoming

Oct 16-18 1973

23 SAE 740165 Lycoming’s LTS 101 Engine Design by J. Moore & E. Pease Avco Lycoming

Feb 25-Mar 1 1974

24 FAA-ADS-59 A Study of Twin-Engine Airplane Propeller Interconnection – Final Report

Jan 1966

25 Report TAR-TR-625 The Aerodynamic Loading on Streamlined Ducted Bodies by Gary R. Hough Contract# Nonr-2859(00) THERM

Dec 1962

26 Propulsion Prospects by R.H. Weir – The Aeronautical Journal of the Royal Aeronautical Society

Nov 1969

27 General Airscrew Applications to VTOL Propulsion THERM

May 16-17 1961

28 Miscellaneous Propeller Papers Various 29 Tandem Air Propellers II by E.F. Lesley Undated 30 NACA TN No. 322 The Effect of the Wings of Single

Engine Airplanes on Propulsive Efficiency as Shown by Full Scale Wind Tunnel Tests

Oct 1929

31 NACA TN No. 333 Test of an Adjustable Pitch Model Propeller at Four Blade Settings

Feb 1930

32 NACA TN No. 562 Experimental Investigation of Aircraft Propellers Exposed to Oblique Air Currents

Apr 1930

33 NACA TN No. 677 Tests of a Contra-Propeller for Aircraft Nov 1938 34 NACA TN No. 689 Tandem Air Propellers Feb 1939 35 NACA ARR No. L4E22 Wind-Tunnel Tests of Dual-

Rotating Propellers with Systematic Differences in Number of Blades, Blade Setting, and Rotational Speed of Front and Rear Propellers

May 1944

36 NACA ARR No. 4H26 An Experimental Investigation of the Thrust and Torque Produced by Propellers Used as Aerodynamic brakes

Aug 1944

37 NACA ARR No. ACR No. L5A11 The Effect of Trailing-Edge Extension Flaps on Propeller Characteristics

Jan 1945

38 NASA TN D-318 A Wind-Tunnel Investigation of Three Propellers Through an Angle-of-Attack Range from 0o to 85o

Apr 1960

203

39 NASA TN D-1774 Aerodynamic Characteristics of a Full-Scale Propeller Tested with Both Rigid and Flapping Blades and with Cyclic Pitch Control

Apr 1963

40 R. & M. No. 1377 Application of Goldstein’s Airscrew Theory to Design by C.N.H. Lock (British Air Ministry)

Nov 1930

41 R. & M. No. 1674 Tables for Use in an Improved Method of Airscrew Strip Theory Calculation by C.N.H. Lock & D. Yeatman (British Air Ministry)

Oct 22 1934

42 Report No. 675 Tests of a Hamilton Standard Four-Way, 21-Inch-Diameter Model Propeller Employing the U.S. Navy Airborne Model Testing Facility Contract# Nonr 1858(14) Princeton Univ.

Apr 1964

43 23LF Small Gas Turbine Propellers with Amendment 1 Hamilton Standard

Undated

44 WADC TR 59-421 Study of Propeller Controls for VTOL Aircraft Applications – Phase I – Determination of Aircraft Configuration and Control Requirements Contract# AF­33(616)-6072

Jun 15 1959

45 Doc 81205 Variable Camber Propeller Performance Investigation Boeing Vertol

Feb 4 1966

46 NASA CR 114399 Advanced general Aviation Propeller Study Contract# NAS2-6477

Dec 21 1971

47 AR# 1023 Generalized Propeller Noise Estimating Procedure – Revision D. Hamilton Standard

Jul 12 1971

48 NASA CR 114289 Advanced General Aviation Propeller Study Contract# NAS2-5885 Hamilton Standard

Apr 1971

49 NASA CR xxx Computer Program User’s Manual for Advanced General Aviation Propeller Study Contract# NAS2-6477 Hamilton Standard

Dec 21 1971

PROPELLERS Conference on Propeller Propulsion(COPP), Apr 22-24 1980

104 1 COPP Application of Propeller Technology to General Aviation Aircraft

Nov 1980

2 COPP Review of Propeller Propulsion Progress up to the 1970’s by Charles Scolatti

C.A. 1980

3 COPP Remarks by David J. Goldsmith of Eastern Airlines C.A. 1980 4 COPP Propeller Drive System Considerations,

Requirements, Design Philosophy, Recommended R&D and Quantification of Benefits by Terry A. Lyons

C.A. 1980

5 COPP The Commercial Aircraft Designer’s View of Propeller Propulsion by Richard Foss

C.A. 1980

6 COPP A Military Aircraft Designer’s View of Propeller Propulsion by Richard Scherrer

C.A. 1980

204

7 COPP Advanced Propeller Potential by Bernard Gatzen Hamilton Standard

C.A. 1980

8 COPP Navy User’s View of Propeller Propulsion by Captain W.A. Finn

C.A. 1980

9 COPP The Commercial Aviation User’s View of Propeller Propulsion by David J. Goldsmith

C.A. 1980

10 COPP Engine Considerations by Robert Neitzel & Robert Hirschkron

C.A. 1980

11 COPP Application of Propeller Technology to General Aviation Aircraft by Cornell Slivinsky

C.A. 1980

12 COPP General Outline and Host Comments by Donald L. Nored NASA-Lewis Research Center

Apr 22-Apr24 1980

13 COPP related Clippings and Articles Various 14 COPP – Photos and Vugraphs C.A. 1980 15 COPP – Congressional Subcommittee Testimony C.A. 1980 16 The World is Round and So Are Propellers Jan 27 1981 17 NASA’s Propfan Progran – The case for Acceleration Undated 18 Propfan C-141 In-Service Demonstration Jan 15 1981 19 Turboprop Study Jan – Jun 1981 20 Lusczak ASD Activities Undated 21 Other Propeller Presentations Various 22 COPP – Miscellaneous C.A. 1980 23 Recommended Plan to Achieve Timely Technology

Readiness of Prop-Fan Propulsion & Airplane Systems Jan 23 1981

24 Report NAPTC-AED-1862 Advancement in Technology for Propellers: State of the Air

Nov 15 1967

25 SP 05A80 Advanced Turboprop Propulsion Technology Oct 1980 26 Quiet 24PF Fiberglass Covered Propeller Blade Hamilton

Standard Nov 17 1975

27 Possibilities for Progress in Gear Technology Mar 28 1968 28 SP 07A77 Prop-Fan Technology Status Report Undated 29 Hamilton Standard – Advanced Propeller Concepts C.A. 1963 30 Hamilton-Standard – Propellers for Advanced V/STOL

and STOL Aircraft C.A. 1968

31 AIAA 79-0610 Aeroacoustic Design of the Propeller by F.B. Metzger & C. Rohrbach Hamilton Standard

Mar 12-14 1979

32 SAE 780995 Prop-Fan Propulsion – Its Status and Potential

Nov 27-30 1978

33 NASA CR 159355 Turboprop Cargo Aircraft Systems Study Phase I Contract# NAS1-15708

Nov 1980

34 PDB 6101 Generalized Method of Propeller Performance Estimation Hamilton Standard

Jun 1963

35 Experimental Verification of Hamilton-Standard Method of Calculating Performance of Propellers in a Shroud

Mar 24 1961

36 Miscellaneous Design Information (Propellers) Undated 37 Propeller Performance Bibliography Jun 21 1973

205

38 Prop Fan Articles C.A. 1972

SMALL TACTICAL AERIAL MOBILITY PLATFORM (STAMP) & Lindenbaum Presentation of 1981

105 1 VTOL Overview Through 1980 C.A. 1981 2 V/STOL Concepts and Developed Aircraft – A Historical

Review by Bernard Lindenbaum - Documents Contract# N00019-78-C-0552

Mar 1981

3 V/STOL Concepts and Developed Aircraft – A Historical Review by Bernard Lindenbaum - Notes Contract# N00019-78-C-0552

Mar 1981

4 Report No. NWC TP 5853 The Alperin Jet-Diffuser Ejector (AJDE) – Development, Testing, and Performance Verification Report Contract# N00123-74-C-0243

Feb 1976

5 Jet Diffuser Ejectors – Miscellaneous Papers C.A. 1973 6 WASP II Program – STAMP – Williams Research Corp. Sep 24 1980 7 Preliminary Systems Design Engineering for a Small

Tactical Aerial Reconnaissance System – Visual (STARS­V) USAAMRDL

Jun 15 1974

8 TN 4008-5 Revision 1 STAMP Operational Concepts, Mission Characteristics and Design Guidance by James G. Martz, III Naval Weapons Center

Apr 1973

9 TN 4008-6 STAMP Technical Survey, Key Parameters and Technical Concepts of Promise by Bradley D. Kowalsky & Scott W. Pitcher Naval Weapons Center

Apr 1972

10 STAMP Documents and Papers C.A. 1974 11 Report No. 1751 Feasibility Study of Small-Rocket Lift

device Contract# DA 44-177-TC-595 Aerojet-General Corp.

Feb 1960

12 Special Report No. 1820 Stability and Control Study of a Small Rocket Lift Device by P.A. Sollow Aerojet

Jul 1 1960

13 Proposal No. R-2622A The Revision and Expansion of the ASD/XR Drone/RPV Mission Analysis Study Univ. of Dayton

Apr 15 1977

14 Proposal No. R-3035 Review of V/STOL Concepts and Developed Aircraft Univ. of Dayton

Feb 23 1978

15 Report No. TR-737 Jet Lift Concepts to Improve Individual Soldier Mobility by A.H. Bohr Thiokol

Jun 3 1959

16 Report No. TR 3355-1 Rocket Jump Belt – A Proposed Experimental Program by A.H. Bohr Thiokol

Aug 1 1960

17 Document No. 74-210824 Test Report – Small Tactical Aerial Platform (STAMP) – Demonstrator Vehicle Static Tests and Tethered Flight Tests Garrett

Mar 19 1974

206

18 Document No. 74-210825 TR –Feasibility Study for Small Tactical Aerial Platform (STAMP) NWC Contract# N00123-73-C-1073 Garrett

Mar 27 1974

19 Proposal for the Development of a Lift-Fan-Stabilized STAMP Vehicle Hydra-Electric Co.

Oct 15 1973

20 Report No. 159-X-36 Preliminary Design Study of STAMP Configurations NASC Contract# N00019-73-C­0519 Piasecki.

Nov 30 1973

SERIES XI: Microfilm, 1950

Box File Description Date

Records of the Prewitt Aircraft Company, Clifton Heights, PA

106 1 History of the Helicopter, Volumes 1, 2, 4, 11, 12, 13, 16 (A to C), 16 (D to Z)

Mar 10, 1950

2 Rotary Wing Aircraft Handbooks and History, Volume 1, Roll 2 History of the Helicopter from its Beginning to the year 1900

Mar 9, 1950

3 Rotary Wing Aircraft Patent Abridgement, Volume 15, 18002 to 2,491,260

Feb 1, 1950

4 Rotary Wing Aircraft History, Volumes 3, 5, 6, 7, 8, 9, 10, 14, 16, 17, 18

Apr 27, 1950

5 Rotary Wing Aircraft History, Volume 3 Apr 26, 1950 6 Rotary Wing Aircraft History, Volume 3 to Volume 18 Apr 26, 1950

SERIES XII: Film, 1938-1977

Box File Description Date

107 1 L-123 – “Spinning and Tumbling Tests of a 1/18-Scale Model of the Ryan X-13 Airplane” and “Drop Tests of a 1/18-Scale Model of the Ryan X-13 Airplane,” (NACA), 35 minutes, Silent/Black & White

Apr. 1956

2 Down-Wash Tests, Eglin AFB, FL, CH-3, HH-53, C-142A Undated 3 W/O 8875, “VJ-101 Briefing Film”, AF Flight Test Center,

Edwards AFB, CA, Color, Silent Undated

4 “CL-757 V/STOL Flying Simulator,” Lockheed, Color/Sound, 9 minutes

Apr. 23, 1965

5 “ESCAPAC,” Douglas Aircraft Comp., 10 minutes, Color/Sound

Undated

6 YAV-8B, Color, 4.5 minutes Undated

207

7 W/O 8875, “VJ-101C (X-2) Telescope Runs,” Tests: Optimization of Auto-Stabilization System in pitch, roll, and yaw,” AF Flight Test Center, Edwards AFB, CA, Color

May, Aug. 1966

8 Prod. 1563, “Scale Model Tests (Langley),” Bell Aircraft Corp.

Oct 10, 1958

9 First Flight, RSAF System 37 Feb. 8, 1967 10 W/O 8219, “STOL Demonstrations DHC-5,” Color Undated 11 JO# 785, “P-1127 (VTOL),” US Naval Missile Center,

Point Mugu, CA, Color, Silent, 35mm Jun. 15, 1967

12 W/O 8875, “DO-31 Briefing Film,” Color c.a.1966 13 “XC-4B Hummingbird II, Quarterly Progress Report No.

9, Oct. 1-Dec 31, 1968,” Lockheed-Georgia, 10 minutes Dec. 1968

14 “XC-4B Hummingbird II Quarterly Progress Report No. 3, 1 Apr. 1967-30 Jun. 1967,” Lockheed-Georgia, 8 minutes

Jun. 1967

15 “XC-4B Hummingbird II Quarterly Progress Report No. 3, 1 Apr. 1968-30 Jun. 1968,” Lockheed-Georgia,

Jun. 1968

16 “XC-4B Hummingbird II Quarterly Progress Report No. 6, 1 Jan. 1968-31 Mar. 1968,” Lockheed-Georgia, 9 minutes, 15 seconds

Mar. 1968

17 “XC-4B Hummingbird II Quarterly Progress Report No. 1, 21 Sept. 1966-21 Dec. 1966,” Lockheed-Georgia, 9 minutes

Dec. 1966

18 “XC-4B Hummingbird II Quarterly Progress Report No. 4, 1 Jul. 1967-30 Sept. 1967,” Lockheed-Georgia, 10 minutes

Sep. 1967

19 “XC-4B Hummingbird II Quarterly Progress Report No. 5, 1 Oct. 1967-31 Dec. 1967,” Lockheed-Georgia, 10 minutes

Dec. 1967

20 “XC-4B Hummingbird II Quarterly Progress Report No. 2, 22 Dec. 1966-31 Mar. 1967,” Lockheed-Georgia,

Mar. 1967

21 “XC-4B Hummingbird II Quarterly Progress Report No. 8, 1 Jul. 1968-30 Sept. 1968,” Lockheed-Georgia, 7 minutes

Sep. 1968

22 XC-4B Hummingbird II Quarterly Progress Report, Lockheed-Georgia, Undated

Undated

23 MS-401-252, “XV-4B Seat Ejection Report, Lockheed c.a.1968 24 XV-4B Ejection Seat Undated

108 1 H-43 Icing Test Shots, 10 troops in Hoist operation, Autorotation landing, Firefight demonstration

1959?

2 Bell Helicopter Company, “Master” 1965 3 “Downwash Survey Test, “ Eglin AFB, FL, Aug 21-Aug

25, 1967, Edited Version, 17 minutes, Color/Silent Aug. 1967

4 Early Attempts and Some Helicopters to mid-1950s, Historical Film Series, Shell Film

Undated

5 AVROCAR (V/STOL Aircraft) (VHS Tape Copy with 16 mm Film)

Undated

208

109 1 UH-1 Annual Report Undated 2 “H43B Huskie Progress Report,” Kaman Aircraft Corp. Undated 3 HU-1D First Flight c.a.1962 4 X-18 Wing Tilt Operation – Progress 1958 5 Sikorsky “Flying Crane Movie,” 20 min. Jul. 1959 6 “Know Your Iroquois,” Bell Helicopter Comp., 32 min.

Color/Sound Undated

7 W.O. 8232, “Avro Car Model,” Color, Approx. 20 min Mar. 1959 8 Unidentified Boeing Vertol film Dec. 1963 9 “How the XV-4A Augmented Throst System Works” Undated

110 1 “Vision Achieved,” Boeing Vertol Division, Color/Sound, 15 min.

Nov. 1966

2 Springboard for Science? Undated 3 Air Slew Missile Tests in PWT Undated 4 W.O. 698 D.C. Reel 5, Silent Color Print N.C. Undated 5 Joint Flight Test Group, AF Flight Test Center, Edwards

AFB, CA, Color 2 Oct. 1967

6 “Final Flight Test Report X-13 Jan. 1957-Jul. 1957,” Ryan Aeronautical Comp., Color/Sound, 12 min.

Jul. 1957

7 D.O. 31, V/STOL, Color Undated 8 Unidentified Undated 9 Sikorsky CH-54A, Vietnam c.a.1967 10 Unidentified 1968 11 S-64 Ship Trainer Demo, Color, 10 min. Undated 12 “Two Decades of V/STOL,” Ryan Aircraft Comp., Color,

Sound, 14 min. (Out take?) Undated

13 Unidentified Undated 14 Aerodyne in der Flugerprobung, 9 min. 35 sec. 1972 15 MP-223, “XV-4A Hummingbird,” Lockheed-Georgia

Company, Color/Sound, 12 min. Undated

16 “Rigid Rotor Concept,” Lockheed Company, Color/Sound, 7 min.

Aug. 1965

17 T58 Engine Manufacturing, General Electric Undated 18 “VERTOL V-76 Progress Report Undated 19 XV-4A Hummingbird, Camera Position Master Undated 20 X-19 Flight, Aerial Camera, Curtiss-Wright VTOL

Systems Division, Color Aug. 1965

21 “Last Half of Flight Phase Test, Test #3 & #4”, Ryan Aeronautical Company. Color, Silent,

c.a.1966

22 Unidentified Undated 23 WCBS Radio Help-ocopters, Color Apr. 1967 24 “Hueycobra,” Bell Helicopter Comp, Color/Sound, 8 min. Undated 25 “Vertical Take Off and Landing Flight 54 & 55,” Ryan

Aeronautical Comp., B/W, Silent Apr. 1957

209

26 “X-13 First Hovering Flight,” Ryan Aeronautical Comp., Color/Silent

May 1956

27 “X-13 Hook on to Cable,” Ryan Aeronautical Comp., Color/Silent

Jul. 1956

28 “Waffen system KAD Korps Aufklarungs Drohne,” Dornier PR, 10 min. 20 sec.

c.a.1973

29 Unidentified (no case) Undated

111 1 74/W-12 97010, Aerospace General Helo, Color c.a.1974 2 Unidentified Undated 3 XV5A, XC142 Undated 4 Summary of Ground and Air Tow, Sikorsky Aircraft, Air

Material Command, B&W, Silent, 18 min. Undated

5 Unidentified Undated 6 Unidentified Undated 7 Radio 88 Undated 8 HU-1A Annual Progress Report, Bell Helicopter Corp.,

Color/Sound Undated

9 Rigid Rotor Developments, Lockheed California, Color/Sound, 4 min.

Undated

10 Unidentified Undated 11 V/STOL Aircraft Developments, Air Material Command,

B&W, 27 min. Undated

112 1 W.O. 72-800, C-135 Laser Taff Test #2 Nov. 1972 2 X-142 Hover Over Patrol Box & STOL Landing (Edwards

AFB?), Color/Silent c.a.1966

3 5” Folding Prop Rotor Model Wind tunnel Test, Bell Helicopter Comp., Color/Silent, 5 min

Feb. 1970

4 XC-142A Flight #29, #2 Airplane, Color/Silent c.a.1965 5 XC-142 #929 Test, Desert Landing Attempt, AF Flight

Test Center, Color, Mar. 1966

6 SAAB Undated 7 Joint Flight Test Group, AF Flight Test Center, Color Oct. 1967 8 Distortion Patterns c.a.1968 9 Unidentified Undated 10 P41C-COA, TC-427 Undated 11 Data on Investigation of the Effects of Airframe Design on

Inlet Flow Fields by Constant Prokop, Fairchild Republic Division

Undated

12 P41C-COA, TC-427 Undated 13 Hoverbuggy, North American Aviation, Color/Silent, 1

min c.a.1964

14 Slides for Japan DEA Briefing Jul. 1966

113 1 SPR 36-70, Human Engineering Long Line Loiter, Color Undated

210

2 Drops to Small Sites Undated 3 Nichols Design Session, 8mm film Undated 4 SFR – Mother/Daughter, Color Apr. 1968 5 C-130 and L-286 Mother & Daughter Program, Lockheed

Company, 16 min. Undated

6 L-286/130 Proximity Flying, Lockheed Company, 12 min. Undated 7 Helicopter Tow Range Extension Undated 8 Aerocrane Test, Armed Forces Day Apr. 1977 9 AHS X-22A Undated 10 Kellett YO-60 & YG-1B Jump Take Off, Color Undated 11 C-3 Spot Landings, Jump Take Off Undated 12 Progress In VTOL, Report #2, Boeing VERTOL Division,

B&W, Sound, 5 min. Undated

13 The U.S. Army VZ-2 Tilt-Wing Research Aircraft, Boeing VERTOL Division, Color/Silent, 10 min.

Undated

14 XC-142, XV-5, X-19 Undated 15 Tri-Service Accidents Undated 16 Unidentified (not on reel) Undated 17 Go Patrol Excerpts Undated 18 Early GIROs Undated 19 Progress in VTOL, #3, Boeing VERTOL Division,

B&W/Sound, 8 min. Undated

20 German (Focke) Rotary Wing Kite Undated 21 Autogiro (Not on Reel) Undated 22 XR-3 (?) Undated 23 Kellett Undated 24 US AAC Autogiro Unite Graduation Exercises at Patterson

Field, Fairfield, OH plus Series of Scenes of five Kellett YG-1B Autogiros taxiing on ramp and take-off

c.a.1938

25 Unidentified Undated

114 1 XC-142 T.O. & Landing, 20 Palms, Color Mar. 1966 2 XC-142 Downwash Tests at Eglin AFB Undated 3 XC-142 #924 Multi Air Drops Oct. 1966 4 Dummy Rescue Pick-Up, XC-142A, Color/Sound, 5 min. Undated 5 XC-142A Undated 6 Stencil Kit NATC Test Undated 7 XV-4B Escape May 1968 8 Gelac (XV4B Hummingbird) Status Report XV-4B,

Lockheed –Georgia Company, Color/Sound, 4 min. Oct. 1968

9 Gelac (XV4B Hummingbird) Status Report XV-4B, Lockheed –Georgia Company, Color/Sound, 4 min.

Oct. 1968

10 XV4B Tzxi & 1st Flight, T/O & Landing, 4 min. Undated 11 Gelac (XV4B Hummingbird) Status Report XV-4B,

Lockheed –Georgia Company, Color/Sound, 4 min. Oct 1968

211

12 XC-142 Documentary, Paris Air Show, Color/Silent, 17 min.

Undated

13 XC-142A TAC Demo at Eglin Air Force Base, Color/Silent, 12 min.

Oct. 1966

14 XC-142 Category II Operational Suitability Tests, Color/Sound, 19.5 min.

Undated

15 Comparative Downwash and Simulated Forest Rescue, Color

Undated

16 Ground Damage Film, Color/Sound, 19 min. Undated 17 AVROCAR Progress Report #2, Color/Silent Undated 18 XC-142A Sand Operations at Edwards AFB, Silent Undated 19 V41A-77A Test Dec. 1974 20 Bell XF109 Mock Up & Free Flight Test in Wind Tunnel Undated

115 1 Focke-Achgelis, Large Twin Rotor, Focke-Achgelis Kite, R-6, F-5

Undated

2 Mother/Daughter, C-130 and Lockheed 286 (Unedited air­to-air)

Mar. 1968

3 AFSS Tactical Usage Undated 4 Flying Lifeboat (Coast Guard) Undated 5 Film Clips (Historical), VS-300 through CH-53 (Jolly

Green) Undated

6 “Three if by Air,” 33.55 min. Undated 7 Battlefield Pegasus, Boeing Vertol Division, Color/Sound,

12 min. Mar. 1967

8 Lockheed Topped Rotor, Retractable Rotor Undated 9 XFY-1, Convair newsreel release film Jan. 1957 10 XFY-1 “POGO” Hover Test, Convair, San Diego, Color 1954 11 Kellett YO60 and YG1B Gregory Jump-Off, Color Undated 12 Rigid Roto Acrobatics, Lockheed California, Color/Sound,

9 min. Undated

13 Bell Aero D-188, Preliminary Progress Review, Bell Aircraft Corp.

Undated

14 Staff Film Report Submission, 14-41-67, Color Mar. 1967 15 X-13, Portion removed from history film and replaced with

more complete hook on sequence Undated

16 No Man Expendable, Sikorsky Aircraft, Color, 12 min. Undated 17 W-14-CL, Color/Silent Undated 18 Model 48 Undated 19 U of Maryland, XV-48 Wind tunnel Tests, Tufts & Water Undated 20 Stowed Rotor ½ Span Model, Princeton Test, Boeing

Helicopters, Color/Silent Undated

21 1966 AFA Briefing, Stabilized vs Unstablilized Tests, Douglas Aircraft, Color/Silent

1966

22 AFFDL Air Slew Missile, Hughes Model Undated 23 Aftermath of Harrier Crash Undated

212

24 Bell XV-15, Clip removed from Bell film Undated

116 1 Flight Tests of 1/5 Scale Model of the Ryan X-13 Airplane, Color/Silent, 15 min.

c.a.1961

2 “GADS” Graphic Airfield Damage Simulation), McDonnell Douglas, Color, 12 min.

1980

3 X-14 Documentary, Bell Aircraft Corp. Undated 4 Wings for the Ground Commander, Boeing VERTOL

Division, Color/Sound, 16 min. Mar. 1967

5 Rigid Rotor Revolution, Lockheed California, Color/Sound, 16 min.

Mar. 1966

6 Pan Am Bldg Roof? Undated 7 Construction by ‘Copter,’ Sikorsky Aircraft, Color/Sound,

19 min. 18 sec. Undated

8 Vought-Flying Pancake, V-173 STOL, 1942 (Navy), Prototype (XFSU-1), Flew 130 hours of testing

Undated

9 Composite XV-4B Undated 10 “Vertability,” Intro to American Helicopter Society’s first

film for industry, premiered at 23rd Annual National Forum 1967

11 Balzac Flight Test, Boeing Aircraft, Color/Silent Oct. 1965 12 Navy Accident Undated

117 1 Ryan XV-5A Progress Report Jul. 1964 2 Qualitative Assessment, 17 min. Undated 3 X-13 Used in Combat (Korea?), Also, Bell 42 Undated 4 XH-17? Undated 5 YH-40 Annual Report, Color/Sound Undated 6 Demonstration of Kellett YO-60 Autogiro, Silent Undated 7 V/STOL History Film, Non-Helicopter VTOL Aircraft Undated 8 Sikorsky S60 Sky Crane? Undated 9 X-13 Film 1955 10 XV-15 Flight Update, Bell Helicopter, 11 ½ min. Undated 11 XV-3 Summary Report, Color/Sound Undated 12 XR-3 c.a.1975

118 1 X-19, X-22, XC-142 (May be mold damaged) Undated 2 Bendix – 1 place and 5 place; XHRP-1 and Franks original

PV-1 (May be mold damaged) Undated

119 1 XH-17 Upside down, PV-3 Color; Other Miscellaneous Clips

Undated

2 The Evolution of Airlift, Color, 21 min. 40 sec. Undated 3 Propulsion for Vertical Flight, Vertical Flight Foundation

film, Color/Sound, 13 ½ min. Undated

4 H$3B Huskie Progress Report II, Kaman Aircraft Corp., Color/Sound, 20 min.

Undated

213

5 Charlies Choppers SDQP Undated 6 The Bell Helicopter (Bell Early Helicopters) Undated 7 XV-4B Hummingbird II Final, Report, Lockheed-Georgia,

Color/Sound, 19:05 min. Jun. 1969

8 Joint Flight Test Group, Color Oct. 1967 9 Pitcairn Autogiro Development Dec. 1973 10 SAAF: Viggen – fpl37 (English version of Swedish film),

17 min 1970

11 Unidentified Undated 12 Unidentified Undated

VHS Tapes 120 1 LTA 20-1 Development Summary, Program #3, 7 min.;

Walter Cronkite’s Universe “Airship Feature Interview,” 12 min.

Dec. 1981; Jun. 1982

2 Clyclo Crane, Tillanook, OR and Powered Balloon, Astoria, OR

Undated

3 Geared Flap Model Flight Films Undated 4 French – Alar Volant Choppers Undated 5 Projecting Power from the Sea, a presentation of the Navy

League of the United States in Association with Hughes Aircraft Company

Undated

6 O-Wing VTOL Undated 7 Air Force TOWS (“Hat”), Washington, D.C. (Video

Original Copy of Lindenbaum) 12 min. May 1998

8 Logging with Helicopters (From Brinkley U.S. Forest Service)

1986

9 Cessna’s Helicopter Adventure, 1 hr. 49 min Undated 10 Excerpts of V/STOL History Undated

214