UNCLASSIFIED AD 268 412 - DTICNOTICES When Governuent drawings, specifications, or other data are...

UNCLASSIFIED

AD 268 412

ARMED SERVICES TECHNICAL INFORMATION AGENCYARLINGTON HALL STATIONARLINGTON 12, VIRGINIA

UNCLASSIFIED

NOTICE: When government or other drawings, speci-fications or other data are used for any purposeother than in connection with a definitely relatedgovernment procurement operation, the U. S.Government thereby incurs no responsibility, nor anyobligation whatsoever; and the fact that the Govern-ment may have formLlated, furnished, or in any waysupplied the said drawings, specifications, or otherdata is not to be regarded by implication or other-wise as in any manner licensing the holder or anyother person or corporation, or conveying any rightsor permission to manufacture, use or sell anypatented invention that may in any way be relatedthereto.

C\.SD TECHNICAL NOTE 61-117PART II

N.

MECHANICAL PROPERTIES, INFORMATION PROCESSING SYSTEM

C~%

C 0 Fatigue of Metals(; t

CORROSION

ANDHEAT RESISTANT METALS

SECTION I

I / /

Contract AF 33(616)-7238 November 1961S.A. 1(61-1094)S.A. 2(62-479)

BELFOUR ENGINEERING CO. SUTTONS BAY, MICHIGAN

NOTICES

When Governuent drawings, specifications, or other dataare used for any purpose other than in connection with adefinitely related Government procurement operation, theUnited States Government thereby incurs no responsibilitynor any obligation whatsoever; and the fact that thegovernment may have formulated, furnished, or in any vaysupplied the said drawings, specifications, or other data,is not to be regarded by implication or otherwise as inarty mamer licensing the holder or any other person orpatented invention that may in any ry be related thereto.

ASD TECHNICAL NOTE 61-117PART II

M::CHANICAL PROPERTIESINFORMATION PROCESSING SYSTEM

Fatigue of Metals

CORROSIONAND

HEAT RESISTANT METALSSECTION I

Contract AF 33(616)-7238 November 1961S.A. 1(61-1094)S.A. 2(62-479)

BELFOUR ENGINEERING CO. SUTTONS BAY, MICHIGAN

FOREWORD

The graphic displays of metals fatigue data presentediv this report have been prepared by the BELFOUR ENGINEERINGCOMPANY under U.S.A.F. Contract No. AF33(616)-7238, S.A.1(61-1094), and S.A.2 (62-479). This contract was initiatedunder Project No. 7381, "Development of a Materials PropertyData Processing System", Task No. 73812. Administration of theproject is under the direction of the Applications Laboratory,Directorate of Materials and Processes, AeronauticalSystems Division, Wright-Patterson Air Force Base, withDon M. Ingels, Lt/USAF acting as project engineer.

This report is one of a. series being prepared for periodicdissemination.

ASD TN - 61-117 Pt. II

The graphs presented herein display metals fatigue information from varioussources of published and unpublished test reports which have been processedad regenerated through a seni-autoiatic data processing system. Each seriesor set of graphs contain descriptive information (legends) which identifiesthe material, test procedure, test conditions and the most significant testmd/or material variables associated with 'the plotted data. The data displayedin each set of graphs is intended to answer very general "queastions" and toserve "a a guide ,to further invest igation of specific areas within theSubject presented.

PUDBLCATION ZV3XIW

This report has been reviewed and is approved.

IMR To CIIANDUR:

D. A. ShinnChief, Materials Inforumation branchApp lication LaboratoryMaterials Central

ASD-TN-61-117 Pt II iii

TAKE OF CONTENTS

Page

Introduction I

Graph Sumary, Search 505 2

S/N Graphs or Graph Series of Corrosionand Heat Resistant Materials Tested at Room andElevated Temperatures. Unnotched specimens.

Graph Number

1 (A - C) Multimet N-155 (AMS 5768) 3

2 Timken 16-25-6 (AMS 5727) 7

3 (A & B) Lapelloy 311 9

4 (A & B) Stainless Steel 403 12

5 S-816 (AMS 5534) 15

6 (A & B) Inco SHS - 260 17

7 (A - D) S-816 (AMS 5765) 20

8 GMR- 235 25

9 (A & B) UDIMET 500 27

10 (A & B) RC - A55 Ti Alloy 30

11 Titanium Alloy Ti 140 A (AMS 4923) 33

12 (A & B) 6% AL, 4% V, Titanium Alloy 35

ASD TN-61-117 Pt. II iv

INTRODUCTION

This is one of a series of reports presenting compilations of testresults pertaining to fatigue of metals,

The information contained in each set of graphs is the result of arelatively general "question" asked of a semi-automatic data processingsystem which stores, processes and regenerates the information inthe requested form. More specific and detailed presentations andanalyses are usually possible. These are available upon request. Thegraphic form in which this information is presented is only one ofvarious types of output of which this mechanized system is capable.Tabulations and listings may also be generated by the system.

These data are intended to assist in the determination of reliable andefficient materials propertieF. The information contained hereinshould be used with due consideration to applicable specificationsand established organizational procedures.

All graphs are labeled with a "search number". These serve toidentify a broad block of information associated with a particular(internal) data processing pactern. Craph numbers are assigned insequence within atq search for the purpose of separating andidentifying sub-groups of useful information. There is no re-quirement for graphs in any number sequence to have any relationshipother than being the produt of the same search., Alphabeticcharacters following a common graph number are used to identify aseries or set of graphs which are related. Subsequent graphs withina, series (bearing a common. graph number) are used to indicate effects andinteractions associated with some obvious variables. The unlimitednumber of combinations available for display and analysis dictates thatthese presentations be limited to relatively gevneral subject matter.Detailed studies car, b,2 performed on request.

A legend on each graph describes the materiil, test type and othervariables necessary to identify the plotted data. rhe reference list for.ach graph set follos the last graph of the set.

ASD IN-61-117 Pt 'I 1

GRAPH SUMMARY SEARCH 505S/N Diagrams of Corrosion and Heat Resistant Materials tested at room andelevated temperatures. All specimens unnotched.

Graph Ult. Tensile Test Type ofNumber Material IdentifiLation Strength, KSI Temperature Loading

1A Multimet N-155, AMS 5768 119-1 6 Room Temp. Bending

1B Multimet N-155, AMS 5768 119-126 1000 - 15000F Bending

IC Multimet N-155, AMS 5768 119 Room Temp. & Rotary Beam1200 - 1500 0 F

2 Timken 16-25-6, AMS 5727 120 Room Temp. & Axial1200 F

3A Lapelloy 311 136 900 - 11000F Axial

3B Lapelloy 311 129 Room Temp. & Rotary Beam_ 9000 ,,

4A Stainless Steel 403 141 Room Temp. & Axial500 - 9000F

4B Stainless Steel 403 129 Room Temp. & Rotary Beam700 - 900 _F

5 S-816, AMS 5534 147 Room Temp. & Rotary Beam1350 16500 F

6A Inco SHS - 260 260 500- 8000F Axial

6B Inco SHS - 260 129-132 Room Temp. Rotary Bleam

7A S-816, AMS 5765 147 Room Temp. & Axial1350 - 16500F

Y6 S-8[6, AMS 5765 Room Temp. & Beading' Hardness; 1200 - 1500 °0Rockwe 11

7C S-81.6, AMS 5765 ) C 26 1200 F Bending

7D S-816, AMS 5765 N.A.* 1200 - 1500 0 F Rotary Beam

S GMR - 235 N.A. Room 0 Temp. & Axial______ ___ ___ ___ _ _______ ___ 1200 F

9A UDDIEl 500 N.A. Room Temp. & Bending1200°F

9B UDIMET 500 N.A. 18000F Bend ing

IOA RC-A55 Ti Alloy 76, 86 Room Temp. Rotary Beam125 6: N.A.

lOB RC-A55 Ii AIlov 76, 86 Room iemp . Rotary Beam125 & NA.

11 MIS 4923, "[ 140 A 130- 150 oom T-mp. & Rotary Bearn00 04

-x T ,VL - - a i, 136 &170 Room Tuip. . aIal750°F

12B i.'. AL- 4 V-[i Allox 140 Room iir't,. RoU,;ry bcam

*N.A. IndiiLJ , c i foination lot ,va lble from original sourc, docoment

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REFERENCES ---- GRAPH SERIES NO. l(A-C), SEARCH 505

ReferenceNumber Reference

058 Ferguson, R.R.; "Effect of Surface Finish onFatigue Properties at Elevated Temperatures inLow Carbon N-155 with Grain Size ASTM-1" NACARM E51D17 (June 1951)

059 Ferguson, R.L.; "A Further Investigation of theEffect of Surface Finish on Fatigue Propertiesat Elevated Temperatures". NACA 3142 (March 1954)

061 NACA Subcommittee on Heat Resisting Materials,"Cooperative Investigation of Relationship BetweenStatic and Fatigue Properties of Wrought N-155Alloy at Elevated Temperatures". NACA TN 3216(April 1955) NACA RM 51A04 (March 1951)

069 Anon, "Room and Elevated Temperature FatigueCharacteristics of Ti-641-4V". Technical ServiceDepartment, Titanium Metals Corporation of America(December 1957).

ASD TN-61-117 Pt. 11 6

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092 Vitovec, F.H.; lAzan, B..J.; "Fatigue, Creep, anidRupture Properties of Heat Resistant Materials",WADC TR 56-181, ASTIA AD 97240 August 19.56)

ASD TN-61- 17 Pt, 11 8

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070 Podnieks, E.R.; Lazan, B.J.; "Damping Elasticityand Fatigue Properties of Titanium Alloys, HighTemperature Alloys, Stainless Steels, and GlassLaminate at Room and Elevated Temperatures".WADC TR 56-37 (March 1956)

092 Vitovec, F.H.; Lazan, B.J.; "Fatigue, Creep, andRupture Properties of Heat Resistant Materials",WADC TR 56-181, ASTIA AD 97240 (August 1956)

ASD TN-61-117 Pt. II

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REFERENCES ---- GRAPH SERIES NO. 4 (A & B), SEARCH 305



092 Vitovec, F.H.; Lazan, B.J.; "Fatigue, Creep, andRupture Properties of Heat Resistant Materials".WADC TR 56-181, ASTIA AD 97240 (August 1956)

ASD TN-b1-117 Pt. II 14

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ASD TN-61-117 Pt. II 16

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REFERENCES ---- GRAPH SERIES NO. 6 (A & B). SEARCH 505

ReferenceNumber ReferecLce

031 Thomassen, L., Sinnott, M.J., Demmler, A.W., Jr.,"The Influence of Surface Treatment on the FatigueProperties of Titanium and Titanium Alloys",WADC TR 53-437, Part 2 (October, 1954).

036 Muvdi, B.B., Sachs, G., Klier, E.P., "DesignProperties of High-Strength Steels in the Presenceof Stress Concentrations, Part II, Axial LoadFatigue Properties of High-Strength Steels",WADC TN 56-395, ASTIA No. AD 110619 (December, 1956).

ASD TN-61-117 Pt. II 19

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REFERENCES ---- GRAPH SERIES NO. 7 (A-D), SEARC 505


019 Smith, Frank C., Brueggeman, William C., andHarwell, Richard H., "Comparison of Fatigue Strengthsof Bare and Alclad 24S-T3 Aluminum Alloy SheetSpecimens Tested at 12 to 1000 Cycles per Minute",NACA TN 2231 (December, 1950).

059 Ferguson, R.L.; "A Further Investigation of theEffect of Surface Finish on Fatigue Properties atElevated Temperatures". NACA 3142 (March 1954).

119 General Electric, "High Temperature Fatigue Testing".Report R-452015A (December 1946).

ASD TN-61-117 Pt. 11 24

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121 Vitovec, F.H.; "Fatigue, Creep, and RuptureProperties of the Alloys UDII4ET 500. HASTELLOYR-235 and GMR-235". WADO TR 58-340 (Oct. 58)

ASD TN-6i-117 Ft. ITT 26

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110 General Electric Co. "The Effect of ProtectiveCoatings on the Cantilever Bending FatigueProperties of Udimet 500 Alloy @ 1800 F".MLER-WCLT L-59-11 (April 1959)

121 Vitovec, F.H.; "Fatigue Life of 2024-T4Aluminum Alloy at Low Stresses" WADC TN 56-433& ASTIA AD 113355 (October 1956)

ASD TN-61-117 Pt. Ii 29

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074 Romualdi, J.P.; D'Appolonia, E.; "Research &Development of Effect of Range of Stress andPrestrain on Notched Specimens of Titanium andits Alloys". Carnegie Institute of Technology(October 1953).

ASD TN-61-117 Pt. 1I 32

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ReferenceNumber References

070 Blatherwick, A.A.; and Lazan, B.J.; "FatigueProperties of Extruded Magnesium Alloy ZK60Under Various Combinations of Alternating &Mean Axial Stresses". WADC TR 53-181 (Aug. 1953)

084 Kaufan, J.G.; Crum T.G.; D'Appolonia, E.;"Correlations of the Mechanical Properties ofTi-150A, RC-130A, RC-130B Ti-Alloy & Ti-75ATitanium Alloys". Carnegie Institute ofTechnology (April 1954)

ASD TN-61-117 Pt. II 34

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069 Anon, "Room and Elevated Temperature FatigueCharacteristics of Ti-641-4'. Technical ServiceDepartment, Titanium Metals Corporation ofAmerica (December 1957)

098 Cummings, H.N.; "Investigation of MaterialsFatigue Problems". Curtiss-Wright Corporation,Contract No. AF33(616) 2876, Report Numbers I to10 (April 1955 through October 1956)

ASD TN-61-117 Pt. II 37

UNCLASSIFIED AD 268 412 - DTICNOTICES When Governuent drawings, specifications, or other data are...

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