FINAL PROGRAM AS OF 1-23-14 - U.S. Advanced Ceramics
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Final Program 38 th Annual Conference on Composites, Materials and Structures (U.S. Citizens Only / ITAR Restricted Sessions) No Photographs Permitted www.advancedceramics.org/conference
Transcript of FINAL PROGRAM AS OF 1-23-14 - U.S. Advanced Ceramics
Final Program
38th Annual Conference on
Composites, Materials and Structures (U.S. Citizens Only / ITAR Restricted Sessions)
No Photographs Permitted
www.advancedceramics.org/conference
Final Program
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Program at a Glance
Sunday Evening, January 26, 2014
6:00-9:00pm Pre-Registration (Convention Center Lobby)
Complimentary Refreshments
Monday, January 27, 2014 Tuesday, January 28, 2014
Morning Session 8:40-11:40 Plenary Session
Afternoon – Two (2) Concurrent Sessions
1:30-4:40 Session 1: Ceramic Matrix Composites 1 1:30-5:00 Session 2: Extreme Environment Materials 1
Afternoon/Evening Activities Pavilion
12:00-1:30 Exhibitor Set-up 5:00-7:00 ITAR Restricted Expo and Networking Social
Morning – Two (2) Concurrent Sessions
8:30-12:00 Session 1: Ceramic Matrix Composites 2 8:30-10:00 Session 2: Carbon-Carbon Materials
Afternoon – Two (2) Concurrent Sessions 1:30-4:20 Session 1: Ceramic Matrix Composites 3 1:30-5:20 Session 2: Ablator Materials
Evening Activities Pavilion
5:00-7:00 ITAR Restricted Expo and Networking Social 7:30-8:30 Exhibitor Breakdown
Wednesday, January 29, 2014 Thursday, January 30, 2014
Morning – Two (2) Concurrent Sessions 8:15-12:00 Session 1: Behavior and Life Ceramic Matrix
Composites 1 8:30-12:00 Session 2: Extreme Environment Materials 2 12:00-1:30 Complimentary Radisson Luncheon or
Lunch on your own - Pavilion
Afternoon Session 1:30-5:00 Session 1: Behavior and Life Ceramic Matrix
Composites 2 1:30-4:00 Session 2: Extreme Environment Materials 3
Program Reviews
Morning – Two (2) Concurrent Sessions
8:15-12:00 Session 1: Behavior and Life of Ceramic
Matrix Composites 3 8:20-11:50 Session 2: Hypersonic Vehicle Materials/
Structural Evaluations 1
Afternoon Session 1:30-5:00 Session 1: Behavior and Life of Ceramic
Matrix Composites 4 1:30-3:00 Session 2: Hypersonic Vehicle Materials/
Structural Evaluations 2
Additional Activities at the Hotel 1:30-5:00 CMH-17 Handbook
Jamaica Meeting Room (off hotel lobby)
Steve Atmur, ATK Space Systems, Rocket Center, WV Email: [email protected]
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MONDAY MORNING, JANUARY 27, 2014 Plenary Session Location: Salons 1 and 2
7:30-8:30am Registration and Continental Breakfast 8:40-8:50am Welcome Remarks by Jay Lane, USACA Chairman 8:50-9:00am Opening Comments by Mark Opeka, Program Chair 9:00-9:40am Development of Advanced SiC-SiC Ceramic Matrix Composites for Aircraft Propulsion
Dr. Sanjay M. Correa, Vice President - CMC Program, GE Aviation, Cincinnati, OH 9:40-10:20am NASA Glenn’s Heritage in Oxidation of Ceramic Turbine Engine Materials
Dennis Fox, NASA Glenn Research Center, Cleveland OH 10:20-10:40am BREAK 10:40-11:20am Ablation Material-Environment Interactions
Charles Powars, St Croix Research, San Jose, CA 11:20-11:40am Composite Materials Handbook-17, Ceramic Matrix Composites
Kaia David, The Boeing Company, Huntington Beach, CA
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MONDAY AFTERNOON – JANUARY 27, 2014 Session 1: Ceramic Matrix Composites 1 Session Chairs: J. Douglas Kiser and Dennis Fox, NASA Glenn Research Center, Cleveland, OH Location: Salon 2
1:35-1:40pm Session Chairs Remarks 1:40-2:00pm Strain Rate Dependent Material Constitutive Model for Impact of 2D Woven Ceramic Matrix
Composites E. J. Klock-McCook and B. Sullivan, Materials Research & Design, Inc., Wayne, PA
2:00-2:20pm Foreign Object Damage Resistance of Ceramic Matrix Composites: Simulation and Post-Test
Data Correlation of Impact Testing C. Iwano, E.J. Klock-McCook and B. Sullivan, Materials Research & Design, Inc., Wayne, PA J. Cuneo and J. Koenig, Southern Research Institute, Birmingham, AL
2:20-2:40pm Ceramic Matrix Composite Fracture Toughness Testing
C. Iwano and B. Sullivan, Materials Research & Design, Inc., Wayne, PA J. Cuneo and J. Koenig, Southern Research Institute, Birmingham, AL
2:40-3:00pm Progress and Plans for CMC Research at NASA Glenn in 2014
J. Grady, NASA Glenn Research Center, Cleveland OH 3:00-3:20pm BREAK 3:20-3:40pm Preliminary Studies on the Development of Engineered Matrices for SiC Fiber Reinforced
Ceramic Composites S. Raj, NASA Glenn Research Center, Cleveland, OH R. Bhatt and M. Singh, Ohio Aerospace Institute, Cleveland, OH
3:40-4:00pm CMC Mixer Nozzle Development in the NASA ERA Project
D. Kiser, N. Bansal and J. Szelagowski, NASA Glenn Research Center, Cleveland, OH J. Sokhey, T. Heffernan and J. Clegg, Rolls-Royce North American Technology, Inc., Indianapolis, IN J. Riedell, ATK COI Ceramics, San Diego, CA S. Atmur, ATK COI Ceramics, Rocket Center, WV S. Haeske, Support Services, LLC, Allendale, MI T. Wyen, Air Force Research Laboratory, Wright Patterson AFB, OH J. Ursic, Zin Technologies, Cleveland, OH
4:00-4:20pm Structural Dynamic Response of CMC Mixer Nozzle Using Laser Vibrometry
T. Wyen, Air Force Research Laboratory, Wright Patterson AFB, OH 4:20-4:40pm High Pressure Turbine Ceramic Matrix Composite Vanes and Rotor Blades
R. Boyle, A. Parikh and V. Nagpal, N & R Engineering Services, Cleveland, OH M. Halbig and J. DiCarlo, NASA Glenn Research Center, Cleveland OH
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MONDAY AFTERNOON – JANUARY 27, 2014 Session 2: Extreme Environment Materials 1 Session Chairs: Eric Wuchina, Naval Surface Warfare Center, Carderock, West Bethesda, MD
Gautham Ramachandran, Lockheed Martin, Palo Alto, CA Joseph Pluscauskis, Materials Research & Design, Inc., Wayne, PA W. Howard Poisl, Raytheon Missile Systems, Tucson, AZ
Location: Salon 1 1:35-1:40pm Session Chairs Remarks 1:40-2:00pm IHPRPT Transition Story on Tungsten Based Non-eroding Solid Rocket Motor Nozzles
L. Matson, Air Force Research Laboratory, Wright Patterson AFB, OH 2:00-2:30pm Near Net Shaped Ta-Carbide Nozzle Liners via Field Assisted Sintering Technology (FAST)
L. Matson, Air Force Research Laboratory, Wright Patterson AFB, OH H. D. Lee, UES, Inc., Dayton, OH J. Singh, Applied Research Laboratory, State College, PA
2:30-3:00pm Low-Erosion and Affordable Nozzles for Advanced Tactical Missiles
J. Pluscauskis, Materials Research & Design, Inc., Wayne, PA 3:00-3:20pm BREAK 3:20-3:40pm Directed Energy Weapon (DEW) High Energy Laser (HEL) Exposure Testing of Selected Aircraft
Materials T. Luce, Northrop Grumman, Aerospace Systems, Advanced Materials & Processes Development El Segundo, CA J. Machan, J. Garcia, R. Bunnell and J. Morais, Northrop Grumman, Aerospace Systems, Space Park, Lasers and Sensor Products, Redondo Beach, CA
3:40-4:00pm Compatibility Studies on MAR-M-247 and Potential Space Nuclear Power Materials
D. Kramer, S. Goodrich, T. Wittberg, C. Whiting and C. Barklay, University of Dayton, OH 4:00-4:20pm Measurement of Surface Catalyzed Recombination Efficiencies by Laser Induced Fluorescence
D. Fletcher, J. Meyers and W. Owens, University of Vermont, Burlington, VT 4:20-4:40pm Oxidation of SiC Thermal Protection Blankets
W. Owens, J. Meyers and D. Fletcher, University of Vermont, Burlington, VT 4:40-5:00pm Design and Analysis of a Composite Case
D. Hladio, D. Caputo and K. Buesking, Materials Research & Design, Inc., Wayne, PA
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MONDAY EVENING – JANUARY 27, 2014
12:00-1:30pm Exhibitor Set-up
5:00-7:00pm ITAR RESTRICTED Expo and Networking Social
LIST OF EXHIBITORS
Carbon-Carbon Advanced Technologies, Inc. Cincinnati Testing Laboratories, Inc. Deltech, Inc. EEMS, LLC Element Materials Technology Free Form Fibers Lancer Systems MATECH Materials Research & Design, Inc. Plasma Processes, LLC Rolls-Royce High Temperature Composites, Inc. SpaceX Specialty Materials, Inc. Starfire Systems, Inc. Ultramet
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EXHIBITORS GUIDE
Company
Company Profile
Booth Number
Plasma Processes Plasma Processes develops, applies and validates engineered materials solutions for thermal & oxidation protection, emissivity, wear and corrosion resistance, in addition to the manufacture of net-shape components for propulsion subcomponents. Plasma Processes serves customers in the government, aerospace/ defense and commercial sectors across a broad range of markets.
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Specialty Materials Specialty Materials produces boron and silicon carbide fibers. Boron is used extensively in aerospace and sporting goods applications. Boron/graphite fiber hybrid preforms are used for selective reinforcement to enhance compression, impact and open-hole compression properties. SiC fibers have outstanding high temperature mechanical properties for increasing strength, stiffness and use temperature of titanium matrix composites, and toughness of ceramic matrix composites.
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Free Form Fibers Free Form Fibers is a US company specializing in laser printing and processing of parallel ceramic monofilaments. This unique technology affords a level of control of fiber diameter, composition, and morphology never before available to the Ceramic Matrix Composite industry. For example, the LP-20SC line of Silicon Carbide is comprised of up to 300 continuous filaments, 20 microns in diameter and of CVD-quality composition. Our unique direct fiber laser printing technology requires no core and produces arrays of fibers that we have demonstrated can be coated with a layer of Boron Nitride and subsequently coated with SiC. Fibers can be made available in tapes of parallel fibers or in tows of continuous filaments appropriately sized for CMC applications.
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Deltech, Inc. Our trademarked motto is, "We Build The Furnace To Fit Your Need"®. Since 1968, family owned and operated Deltech has designed and built standard and custom electric benchtop and production scale furnaces for materials science researchers and manufacturers worldwide. Operating temperatures up to 2000 deg C in air, inert atmospheres, and under positive pressures. Special designs for glass melt applications. Rotary kilns are our newest offering.
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EEMS, LLC Manufacturer and supplier of high temperature materials and ceramic forming polymers.
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Company
Company Profile
Booth Number
Element Materials Technology With a network of over 1500 engaged experts, Element Materials Technology is the recognized leader in materials testing, product qualification testing, and failure analysis
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MATECH MATECH has developed and produces 500 filament ceramic fiber tow of two types of silicon-based fibers, silicon nitride/carbide (SiNC-1400X) and stoichiometric silicon carbide (SiC-1900X) for use in advanced ceramic matrix composites (CMCs). MATECH is a leader in ultra-high-temperature (UHT) CMCs for missile propulsion and aerothermal TPS applications. MATECH manufactures UHT C/ZrOC CMCs. MATECH manufactures SiC-matrix CMCs by PIP, CVI, Hybrid CVI/PIP, and FAST CMC processing. MATECH has a dedicated CVI/CVD facility for both interface coatings and matrix densification. MATECH has a dedicated weaving lab specializing in high modulus ceramic fibers. MATECH is fully integrated, from the manufacture of fibers, weaving of fabric, deposition of interface coatings, and CMC densification.
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Materials Research & Design, Inc.
Materials Research & Design (MR&D) is a small business that provides research and design services to the aerospace materials community. Typical programs at MR&D focus on the simultaneous design of material and structure to optimize component cost, weight, or structural performance. Additional areas of interest focus upon research into the behavior of composite materials and the development of micromechanical models to analyze and understand observed properties. The analytical approach employed by MR&D is based upon a practical understanding of engineering issues founded upon a strong background of theoretical mechanics.
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Carbon-Carbon Advanced Technologies, Inc.
Carbon-Carbon Advanced Technologies, Inc. Pioneering High Temperature Carbon-Carbon composites; deliverable for Flight Programs and Space technologies.
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Ultramet Ultramet is an ISO 9001:2008-certified producer of flight-qualified components, comprised of engineers, scientists, and support personnel, production and R&D facilities particularly suited to the research, development and production of advanced materials including high temperature capability, corrosion- and erosion-resistant materials. Ultramet personnel will be available to discuss your specific materials-related applications.
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Company
Company Profile
Booth
Number
Starfire Systems, Inc. Starfire Systems, Inc (SSI) is a specialty material company focused on Polymer Derived Ceramics (PDC) and its Polymer-to-CeramicTM technology. SSI’s core business is synthesis of silicon-based pre-ceramic polymers and SOL-GEL derived oxide forming materials which are used in polymer matrix composites, oxide and non-oxide ceramic matrix composite fabrication. SSI’s high temperature materials are useful in a variety of applications where durable, lightweight and high temperature ceramics or coatings are required, such as frictional components, electronic components, thermal protection systems, and rocket nozzles. As a raw material and technology system supplier, SSI continues to focus on supporting our manufacturing partners to develop materials and systems that meet the needs of a broader range of customers and end markets.
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Rolls-Royce High Temperature Composites Inc.
Rolls-Royce High Temperature Composites Inc. specializes in the manufacturing of ceramic matrix composites for gas turbine engine, nuclear, rocket propulsion and industrial markets.
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SpaceX SpaceX designs, manufactures and launches advanced rockets and spacecraft. The company was founded in 2002 to revolutionize space technology, with the ultimate goal of enabling people to live on other planets.
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Lancer Systems Lancer is an engineering and manufacturing firm trusted by customers in the defense, aerospace, natural gas and oil industries. The company deploys cutting edge ceramic, fiber optic and composite technologies, developing innovative material solutions that are light weight, innovative and cost effective.
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Cincinnati Testing Laboratories, Inc.
Cincinnati Testing Labs specializes in machining, conditioning, & testing of Advanced Materials including Composite, CMC, PMC, MMC, Elastomers, Plastics, Ceramics and Metallics. Testing is conducted to customer & standard specifications for all forms of mechanical properties testing including static, fatigue, fracture mechanics, & crack propagation. We can test in temperatures ranging from -320 Deg. F up to 2800 Deg. F. in controlled environments. Stop by our booth and speak to us about your testing needs.
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TUESDAY MORNING – JANUARY 28, 2014 Session 1: Ceramic Matrix Composites 2 Session Chairs: Mike Cinibulk, Air Force Research Laboratory, Wright Patterson AFB, OH Jim Steibel, GE Aviation, Cincinnati, OH Location: Salon 2
7:30-8:30am Registration and Continental Breakfast 8:35-8:40am Session Chairs Remarks 8:40-9:00am 2700°F SiC/SiC Composites for Turbine Hot Section Components – AFRL Plans and Programs
A. Katz, Air Force Research Laboratory, Wright Patterson AFB, OH 9:00-9:20am Development of the Next Generation of Ceramic Matrix Composites for Turbine Engines –
2700°F SiC/SiC A. Chamberlain, Rolls-Royce Corporation, Indianapolis, IN R. Shinavski, Rolls-Royce High Temperature Composites, Huntington Beach, CA
9:20-9:40am Effects of Interface Coatings and Fiber Architecture on the Mechanical Properties of SiC/SiC
CMC's K. Newton and D. Berczik, Pratt & Whitney, East Hartford, CT T. Easler, COI Ceramics / ATK, San Diego, CA
9:40-10:00am 2700°F SiC/SiC CMC Development
G. Kirby, J. Steibel and H. Yun, GE Aviation, Cincinnati OH 10:00-10:20am BREAK 10:20-10:40am Improving Matrix Properties of Melt Infiltrated SiC-SiC Composites through Active Fillers
T. Key, C. Carney and K. Keller, UES, Inc., Dayton, OH M. Cinibulk, Air Force Research Laboratory, Wright Patterson AFB, OH
10:40-11:00am Quantifying Amorphous Content of Converted Pre-ceramic Polymers in SiC Fibers and Matrix
M. O'Malley and M. Cinibulk, Air Force Research Laboratory, Wright Patterson AFB, OH T. Key, I. Wolford and K. Keller, UES, Inc., Dayton, OH
11:00-11:20am Modeling Environmental Degradation of SiC Fibers and CMCs
T. Parthasarathy, UES, Inc., Dayton, OH R. Hay and M. Cinibulk, Air Force Research Laboratory, Wright Patterson AFB, OH
11:20-11:40am Monitoring Damage of Pre-Preg MI CMCs with Acoustic Emission and Electrical Resistance
N. Gordon and G. Morscher, University of Akron, Akron, OH 11:40-12:00pm Detection of Porosity in CVI SiC/SiC CMC Material Using Several NDE Methods
P. Khandelwal, Rolls-Royce Corporation, Indianapolis, IN 12:00-1:30pm Lunch on your own
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TUESDAY MORNING – JANUARY 28, 2014 Session 2: Carbon-Carbon Materials Session Chair: Andrew Swanson, Air Force Research Laboratory, Wright Patterson AFB, OH Location: Salon 1
7:30-8:30am Registration and Continental Breakfast 8:35-8:40am Session Chair Remarks 8:40-9:00am Fabrication of Affordable 2D Carbon-Carbon Components
J. Shigley, ATK Aerospace Systems, Brigham City, UT 9:00-9:20am Instrumented C-C Plug for Hypersonic Flight Testing
J. Feie, Air Force Research Laboratory, Wright Patterson AFB, OH 9:20-9:40am Transition and Recession Trends in Carbon/Carbon Nosetip Materials
C. Ralph, Southern Research Institute, Birmingham, AL 9:40-10:00am Self-Starting Carbon-Carbon Scramjet Inlet Design and Manufacturing Z. Gaston, GoHypersonic, Dayton, OH 10:00-10:20am BREAK
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TUESDAY AFTERNOON – JANUARY 28, 2014 Session 1: Ceramic Matrix Composites 3 Session Chairs: Martha Jaskowiak and Dennis Fox, NASA Glenn Research Center, Cleveland, OH Location: Salon 2
1:35-1:40pm Session Chairs Remarks 1:40-2:00pm Design Curve Generation for 3D SiC Fiber Architecture
J. Lang and J. DiCarlo, NASA Glenn Research Center, Cleveland OH 2:00-2:20pm Processing and Properties of 2700ºF SiC/SiC Composites with (CVI+PIP) Hybrid Matrix
R. Bhatt, C. Smith and J. DiCarlo, NASA Glenn Research Center, Cleveland OH 2:20-2:40pm Strength, Creep and Microstructural Characterization of Sylramic, Sylramic-iBN and Super
Sylramic-iBN Fibers R. Bhatt, T. McCue, L. Evans, D. Johnson, T. Casper, D. Gorican and J. DiCarlo, NASA Glenn Research Center, Cleveland OH
2:40-3:00pm Evaluation of Chemical Vapor Infiltration/Slurry Melt Infiltration SiC/SiC Composites for
Aerospace Applications M. Jaskowiak and J.DiCarlo, NASA Glenn Research Center, Cleveland OH R. Bhatt, Ohio Aerospace Institute, Cleveland, OH D. Gorican and M. Cuy, Vantage Partners LLC, Lanham, MD
3:00-3:20pm BREAK 3:20-3:40pm Property Evaluation and Damage Evolution of Environmental Barrier Coatings and
Environmental Barrier Coated SiC/SiC Ceramic Matrix Composite Sub-Elements D. Zhu, M. Halbig, M. Jaskowiak, J. Hurst, R. Bhatt and D. Fox, NASA Glenn Research Center, Cleveland OH
3:40-4:00pm Characterization of SiC and SiC/SiC Composite Joints in Complex Geometries
G. Jacobsen, H. Khalifa, C. Deck, O. Izhvanov, O. Gutierrez and C. Back, General Atomics, San Diego, CA
4:00-4:20pm Ceramic Field, Repair for Structurally Compliant, Dielectric Matched Component Restoration
E. Pope, S. Grandi, K. Ringled and S. Kirkwood, MATECH, Westlake Village, CA R. Batzer, Lockheed Martin Aeronautics Company, Fort Worth, TX
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TUESDAY AFTERNOON – JANUARY 28, 2014 Session 2: Ablator Materials Session Chair: Matt Gasch, NASA Ames Research Center, Moffett Field, CA Location: Salon 1
1:35-1:40pm Session Chair Remarks 1:40-2:00pm Calculation of Effective Material Strengths for 3D Woven Hybrid Preforms and Composites
G. Tiscia, K. Hopp and B. Sullivan, Materials Research & Design, Inc., Wayne, PA S. Kroszner and S. Clarke, Textile Engineering and Manufacturing, Inc., Woonsocket, RI J. Cuneo and J. Koenig, Southern Research Institute, Birmingham, AL
2:00-2:20pm Development of Test Methods for Anisotropic Compliances of 3D Woven Preforms for Ablative
TPS C. Mackie, C. Iwano and B. Sullivan, Materials Research & Design, Inc., Wayne, PA J. Cuneo and J. Koenig, Southern Research Institute, Birmingham, AL S. Kroszner and S. Clarke, Textile Engineering and Manufacturing, Inc., Woonsocket, RI
2:20-2:40pm Recent Arcjet Testing of Phenolic Impregnated Carbon Ablator (PICA) - Highlighting New
Missions Possibilities A. Beerman and M. Stackpoole, NASA Ames Research Center, Moffett Field, CA
2:40-3:00pm Flight Representative Arc-Jet Profile Testing
S. Splinter, N. Mesick, W. Bruce, J. Gragg, NASA Langley Research Center, Hampton, VA M. Kardell, Boeing Technology Services, Berkley, MO
3:00-3:20pm BREAK 3:20-3:40pm Development of Lightweight Ablator Heatshield Assemblies and Manufacturing Techniques
S. Violette and M. Lippold, Fiber Materials Inc., Biddeford, ME 3:40-4:00pm Impact of Radiation Wavelength on Thermal Protection Material Testing
S. White, NASA Ames Research Center, Moffett Field, CA 4:00-4:20pm Arcjet Testing of Advanced Conformal Ablative TPS
M. Gasch, P. Agrawal and R. Beck, NASA Ames Research Center, Moffett Field, CA 4:20-4:40pm Biologically-Derived Photonic Materials for Thermal Protection Systems
S. Johnson and T. Squire, NASA Ames Research Center, Moffett Field, CA M. Gusman, ERC Corporation at NASA Ames Research Center, Moffett Field, CA K. Lau and A. Sanjurjo, SRI International, Palo Alto, CA
4:40-5:00pm Mars Science Laboratory Heat Shield Property Characterization
J. Feldman, NASA Ames Research Center, Moffett Field, CA 5:00-5:20pm Hypersonic Inflatable Aerodynamic Decelerators
A. Calomino, NASA Langley Research Center, Hampton, VA
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TUESDAY EVENING – JANUARY 28, 2014
5:00-7:00pm ITAR RESTRICTED Expo and Networking Social
7:30-8:30pm Exhibitor Breakdown
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WEDNESDAY MORNING – JANUARY 29, 2014 Session 1: Behavior and Life Ceramic Matrix Composites 1 Session Chairs: Craig Przybyla and Larry Zawada, Air Force Research Laboratory, Wright Patterson
AFB, OH and Jennifer Pierce, University of Dayton Research Institute, Dayton, OH Location: Salon 1
7:30-8:30am Registration and Continental Breakfast 8:15-8:20am Session Chairs Remarks 8:20-9:00am KEYNOTE: Environmental Degradation of CMCs in Turbine Engine Environment – A Review
T. Parthasarathy, UES, Inc., Dayton OH C. Przybyla, Air Force Research Laboratory, Wright Patterson AFB, OH
9:00-9:20am Thermochemical Degradation Mechanisms of SiC-Based Ceramic Matrix Composites
B. Opila, University of Virginia, Charlottesville, VA 9:20-9:40am Finite Element-Based Life Prediction Modeling of SiC/SiC Ceramic Matrix Composite Materials
in Oxidizing Environments B. Sullivan, Materials Research & Design, Inc., Wayne, PA
9:40-10:00am Modeling of Oxidation Induced Damage in Ceramic Matrix Composites
J. Ahmad and U. Santhosh, Structural Analytics, Inc., Carlsbad, CA Y. Gowayed, Auburn University, Auburn, AL G. Jefferson, Air Force Research Laboratory, Wright Patterson AFB, OH
10:00-10:20am BREAK 10:20-11:00am KEYNOTE: CMC Applications, Behavior and Model Development Needs
D. Carper, GE Aviation, Evendale, OH 11:00-11:20am Behavior and Life Prediction of SiC/SiC CMC's for Turbine Applications: Environmental Damage
Modeling J. Shi, Rolls Royce North America, Indianapolis, IN
11:20-11:40am Behavior and Life Prediction of SiC/SiC CMCs for Turbine Applications
B. Cox and D. Marshall, Teledyne Scientific and Imaging Co. LLC, Thousand Oaks, CA T. Parthasararthy, UES Inc., Dayton, OH R. Ritchie, University of California, Berkeley, CA M. Vinup and N. Wali, Honeywell Inc., Phoenix, AZ Q. Yang, CompositeMore Inc., Coral Gables, FL
11:40-12:00pm Microstructure-Sensitive Behavior and Life Prediction Modeling of SiC-fiber-reinforced SiC
Matrix (SiC/SiC) Composites for Gas Turbine Hot Section Applications K. Rugg, Pratt & Whitney, East Hartford, CT R. Kumar and G. Srinivasan, United Technologies Research Center, East Hartford, CT
12:00-1:30pm Complimentary Radisson Luncheon or lunch on your own
Location: Pavilion
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WEDNESDAY MORNING – JANUARY 29, 2014 Session 2: Extreme Environment Materials 2 Session Chairs: Eric Wuchina, Naval Surface Warfare Center, Carderock, West Bethesda, MD
Gautham Ramachandran, Lockheed Martin, Palo Alto, CA Joseph Pluscauskis, Materials Research & Design, Inc., Wayne, PA W. Howard Poisl, Raytheon Missile Systems, Tucson, AZ
Location: Salon 2 7:30-8:30am Registration and Continental Breakfast 8:35-8:40am Session Chairs Remarks 8:40-9:00am Evaluation of New Insulator Materials for Solid Propulsion Control Systems
T. Dominick, M. Porter and K. Schoonover, ATK Missile Defense and Controls, Elkton, MD 9:00-9:20am Stress Interaction in Engineered Structural Insulators
D. Caputo and K. Buesking, Materials Research & Design, Wayne, PA 9:20-9:40am Aerogel-Filled Foam Core Insulation for Cryogenic Propellant Storage
L. Weller and B. Sullivan, Materials Research & Design, Inc., Wayne, PA D. Hughes and V. Arrieta, Ultramet, Pacoima, CA
9:40-10:00am Advanced Foam-Based Cryogenic Heat Exchangers
A. Fortini, Ultramet, Pacoima, CA 10:00-10:20am BREAK 10:20-10:40am Refractory Coated/Lined Low Density Structures
G. Tiscia, J. Pluscauskis and K. Buesking, Materials Research & Design, Inc. Wayne, PA P. Valentine, NASA Marshall Space Flight Center, Marshall Space Flight Center, AL J. Shigley, R. Roberts and H. Dovey, ATK Aerospace Systems, Brigham City, UT T. McKechnie, A. Shchetkovskiy, S. O’Dell and K. Murphre, Plasma Processes, LLC, Huntsville, AL
10:40-11:00am Design, Analysis, and Testing of Hyper Velocity Projectile Components
D. Hladio, H. Jensen and K. Buesking, Materials Research & Design, Inc., Wayne, PA L. Thomas and V. Lent, Naval Surface Warfare Center, Dahlgren, VA J. Spain, Southern Research Institute, Birmingham, AL T. Quinzi, ITT Exelis, Rochester NY S. Di Pietro, Exothermics, Inc., Amherst, NH
11:00-11:20am Frost Resistance and Moisture Permeability of C/ZrOC UHT Structural Insulator Material
T. Rosengren, S. Grandi, S. Kirkwood and E. Pope, MATECH, Westlake, CA P. Marchol, Aerojet-Rocketdyne, Sacramento, CA
11:20-12:00am Processing and Properties of Hot Isostatically Pressed HfC, HfB2, and Hf-N Ceramics
D. Ramos and J. Zaykoski, Naval Surface Warfare Center, Carderock, West Bethesda, MD 12:00-1:30pm Complimentary Radisson Luncheon or lunch on your own
Location: Pavilion
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WEDNESDAY AFTERNOON – JANUARY 29, 2014 Session 1: Behavior and Life Ceramic Matrix Composites 2 Session Chairs: Craig Przybyla and Larry Zawada, Air Force Research Laboratory, Wright Patterson
AFB, OH and Jennifer Pierce, University of Dayton Research Institute, Dayton, OH Location: Salon 1
1:35-1:40pm Session Chairs Remarks 1:40-2:20pm KEYNOTE: The Effects of Packing Randomness on Deformation Response and Failure of Fiber
Reinforced Composites A. Waas, University of Michigan, Ann Arbor, MI
2:20-2:40pm Microstructure Gestalt in Ceramic Matrix Composites: Characterization and Simulation
C. Przybyla, J. Simmons and L. Zawada, Air Force Research Laboratory, Wright Patterson AFB, OH S. Bricker and J. Pierce, University of Dayton Research Institute, Dayton, OH
2:40-3:00pm Mechanisms of Crack Deflection at the Matrix-Interphase-Fiber Interface in Brittle Matrix
Continuous Fiber Reinforced Composites M. Braginsky, University of Dayton Research Institute, Dayton, OH C. Przybyla, Air Force Research Laboratory, Wright Patterson AFB, OH
3:00-3:20pm BREAK 3:20-4:00pm KEYNOTE: Multiscale Design System for Life Prediction of Ceramic Matrix Composites
J. Fish, Columbia University, New York, NY; Multiscale Design Systems, LLC, New York, NY 4:00-4:20pm Incorporation of a Composite Progressive Damage User-Routine for Finite Element Analysis of
Components under Complex Stress States P. Croteau, X. Wang, Y. Long, United Technologies Research Center, East Hartford, CT R. Naik, Pratt & Whitney, East Hartford, CT” M. Bak, CAEAi, Middlebury, CT
4:20-4:40pm Impact of Defects and Cracks on the Structural Response of CMCs
U. Santhosh, Structural Analytics, Inc., Carlsbad, CA Y. Gowayed, Auburn University, Auburn, AL T. Smyth, Pratt & Whitney, East Hartford, CT G. Ojard, United Technologies Research Center, East Hartford, CT G. Jefferson, Air Force Research Laboratory, Wright Patterson AFB, OH
4:40-5:00pm FEAMAC-CARES: Current Status of CARES (Ceramics Analysis and Reliability Evaluation of
Structures) and MAC/GMC (Micromechanics Analysis Code/ Generalized Method of Cells) Software Coupling Development Effort N. Nemeth, NASA Glenn Research Center, Cleveland OH
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WEDNESDAY AFTERNOON – JANUARY 29, 2014 Session 2: Extreme Environment Materials 3 – Program Reviews Session Chair: Mark Opeka, Naval Surface Warfare Center, Carderock, West Bethesda, MD Location: Salon 2
1:35-1:40pm Session Chair Remarks 1:40-3:00pm Hafnium-based Materials and Refractory Metal Lined Composites for Missile Propulsion
Systems D. Butts, T. McKechnie, S. O’Dell and A. Shchetkovskiy, Plasma Processes, LLC, Huntsville, AL B. Schulz and G. Thompson, University of Alabama, Tuscaloosa, AL
3:00-3:20pm BREAK 3:20-4:00pm Advanced Needled Carbon-SiC Structural Insulator Materials
W. Shih, Allcomp, Inc., City of Industry, CA
Final Program
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THURSDAY MORNING – JANUARY 30, 2014 Session 1: Behavior and Life of Ceramic Matrix Composites 3 Session Chairs: Craig Przybyla and Larry Zawada, Air Force Research Laboratory, Wright Patterson
AFB, OH and Jennifer Pierce, University of Dayton Research Institute, Dayton, OH Location: Salon 1
7:30-8:30am Registration and Continental Breakfast 8:15-8:20am Session Chairs Remarks 8:20-9:00am KEYNOTE: Stochastic Virtual Test Systems for Continuous Fiber Composites
B. Cox, O. Sudre and D. Marshall, Teledyne Scientific Co LLC, Thousand Oaks, CA H. Bale and R. Ritchie, University of California, Berkeley, CA M. Blacklock, T. Fast, V. Rajan, M. Novak, R. Rinaldi, M. Rossol, J. Shaw and F. Zok, University of California, Santa Barbara, CA B. Do, M. Naderi and Q. Yang, University of Miami, Coral Gables, FL
9:00-9:20am Successes and Challenges in Engineering Ceramic Matrix Composites for Aerospace
Applications A. Bhattacharya, L. Lehman, The Boeing Company, Huntington Beach, CA
9:20-9:40am Flight Environment and Process Variable Modeling of Aeroshell TPS
A. Bhattacharya, V. Heng and J. Embler, The Boeing Company, Huntington Beach, CA 9:40-10:00am Characterization of Residual Microstresses in the Matrix Region of Melt-Infiltrated SiC-SiC
Composites B. Wing, F. Esmonde-White and J. Halloran, University of Michigan, Ann Arbor, MI
10:00-10:20am BREAK 10:20-11:00am KEYNOTE: Modeling Creep of SiC Fibers and Its Effects on High-Temperature SiC/SiC CMC
J. DiCarlo, NASA Glenn Research Center, Cleveland, OH 11:00-11:20am Phenomenological Stress and Damage Model for N312/SiOC CMC
R. Brockman, W. Braisted and G. Strunks, University of Dayton Research Institute, Dayton, OH B. Hauber and J. Gauvin, Air Force Research Laboratory, Wright Patterson AFB, OH
11:20-11:40am Biaxial (Tension-Torsion) Testing of an Oxide-Oxide Ceramic Matrix Composite (CMC)
J. DeRienzo, US Air Force, Los Angeles AFB, CA L. Zawada, C. Przybyla, G. Jefferson, E. Jones and R. John, Air Force Research Laboratory, Wright Patterson AFB, OH
11:40-12:00pm Failure of CMCs Under Biaxial Flexure: Experiments and Simulations
L. Hansen and A. Waas, University of Michigan, Ann Arbor, MI 12:00-1:30pm Lunch on your own
Final Program
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THURSDAY MORNING – JANUARY 30, 2014 Session 2: Hypersonic Vehicle Materials/Structural Evaluations 1 Session Chairs: Anthony Calomino, NASA Langley Research Center, Hampton, VA Larry Hudson, NASA Dryden Research Center, Edwards, CA Location: Salon 2
7:30-8:30am Registration and Continental Breakfast 8:20-8:30am Session Chairs Remarks 8:30-8:50am Status on Materials for Hypersonic Weapons and Systems
K. Davidson, Air Force Research Laboratory, Wright Patterson AFB, OH 8:50-9:10am Advances in Rapid Development and Insertion of Hypersonic Materials (RIDHM)
M. Chen, Air Force Research Laboratory, Wright Patterson AFB, Dayton, OH 9:10-9:30am Innovative Materials & Processes Development for Structurally Integrated Thermal Protection
Systems K. Hopp, Materials Research & Design, Inc, Wayne, PA
9:30-9:50am Design, Fabrication and Testing of a 40x40 Array for Hypersonic TPS
D. Howren, Materials Research & Design, Inc., Wayne, PA 9:50-10:10am Design, Analysis, and Testing of Scale-up Samples for a Structurally Integrated Thermal
Protection System R. Brockman, Air Force Research Laboratory, Wright Patterson AFB, Dayton, OH
10:10-10:30am BREAK 10:30-10:50am High-Temperature Structure Concept Development
K. Hopp, Materials Research & Design, Inc., Wayne, PA 10:50-11:10am Leading Edge and Acreage Thermal Design for HIFiRE Flight 6
Z. Gaston, GoHypersonic Inc., Dayton, OH 11:10-11:30am Evaluation of the Operation Envelop of a Sodium Heat Pipe Cooled Leading Edge
B. Hauber, Air Force Research Laboratory, Wright Patterson AFB, Dayton, OH 11:30-11:50am Arcjet Test Conditions and Fixturing for Refractory Metal Heat Pipe Cooled Leading Edge
E. Klock-McCook, Materials Research & Design, Inc., Wayne, PA 12:00-1:30pm Lunch on your own
Final Program
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THURSDAY AFTERNOON – JANUARY 30, 2014 Session 1: Behavior and Life of Ceramic Matrix Composites 4 Session Chairs: Craig Przybyla and Larry Zawada, Air Force Research Laboratory, Wright Patterson
AFB, OH and Jennifer Pierce, University of Dayton Research Institute, Dayton, OH Location: Salon 1
1:35-1:40pm Session Chairs Remarks 1:40-2:20pm KEYNOTE: Use of Acoustic Emission and Electrical Resistivity to Monitor Damage
Accumulation in SiC-based CMCs G. Morscher, University of Akron, Akron OH
2:20-2:40pm Comparison of Results from Different NDE Techniques from Ceramic Matrix Composites with
Varying Porosity Levels T. Smyth, Pratt & Whitney, East Hartford, CT G. Ojard, United Technologies Research Center, East Hartford, CT U. Santhosh and J. Ahmad, Structural Analytics, Inc., Carlsbad, CA Y. Gowayed, Auburn University, Auburn, AL
2:40-3:00pm Nondestructive Evaluation Method Assessment for Bulk Porosity in Ceramic Matrix Composites
W. Hoppe, University of Dayton Research Institute, Dayton, OH 3:00-3:20pm BREAK 3:20-3:40pm Micromechanics Based Modeling of SiC/SiC Composites
S. Arnold, B. Bednarcyk and E. Pineda, NASA Glenn Research Center, Cleveland, OH S. Mital, The University of Toledo, Toledo, Ohio
3:40-4:00pm Characterization of Fracture in Ceramic Matrix Composites at the Microstructural Length Scale
J. Tracy and S. Daly, University of Michigan, Ann Arbor, MI 4:00-4:20pm Verification of Correlations between Electrical Resistivity and Damage State in SiC-based CMCs
Using Progressive Failure Analysis Y. Xue and F. Abdi, AlphaStar Corporation, Long Beach, CA G. Morscher, University of Akron, Akron, OH S. Choi, Naval Air Systems Command, Patuxent River, MD
4:20-4:40pm Quantitative NDE of CMCs by Microwave Interferometry, Validation Report
K. Schmidt and J. Little, Evisive, Inc., Baton Rouge, LA W. Ellingson, ERC Company, Rancho Dominguez, CA
4:40-5:00pm Foreign Object Impact Damage in Ceramic Matrix Composites
M. Mordasky, R. Kumar and G. Ojard, United Technologies Research Center, East Hartford, CT
Final Program
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THURSDAY AFTERNOON – JANUARY 30, 2014 Session 2: Hypersonic Vehicle Materials/Structural Evaluations 2 Session Chairs: Anthony Calomino, NASA Langley Research Center, Hampton, VA Larry Hudson, NASA Dryden Research Center, Edwards, CA Location: Salon 2
1:35-1:40pm Session Chairs Remarks 1:40-2:00pm Advanced Cooling Technology for High Heat Flux Applications
D. Youchison, Sandia National Laboratories, Albuquerque, NM 2:00-2:20pm Testing of a Hot Composite Design for a Hypersonic Vehicle
J. Gauvin, Air Force Research Laboratory, Wright Patterson AFB, Dayton, OH 2:20-2:40pm Update and New Results: The UTK Inverse Calibration Method for Estimating Surface Heat Flux
Using In-Depth Measurements for TPS’s J. Frankel, University of Tennessee, Knoxville, TN
2:40-3:00pm High Heat Flux Testing with Electron Beams
R. Nygren, Sandia National Laboratories, Albuquerque, NM
Final Program
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Thank You to Our 2014 Sponsors!
Conference Program Chair
Dr. Mark M. Opeka Naval Surface Warfare Center, Carderock Division
Code 617 9500 MacArthur Boulevard
West Bethesda, MD 20817-5700 Phone: 301-277-3963
Email: [email protected]
