Books on the topic 'High-temperature tests'
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Wilkinson, C. High temperature cyclic behaviour of aerospace materials: room temperature validation tests of Ti-6Al-4V. Neuilly sur Seine, France: AGARD, 1994.
Mines, United States Bureau of. High-temperature cyanide leaching of platinum-group metals from automobile catalysts--laboratory tests. Pittsburgh, PA: U.S. Dept. of the Interior, Bureau of Mines, 1991.
C, Moore Thomas. Recommended strain gage application procedures for various Langley Research Center balances and test articles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
DellaCorte, Christopher. Tribological properties of PM212: A high-temperature, self-lubricating, powder metallurgy composite. Cleveland, Ohio: Lewis Research Center, 1989.
Wilkinson, C. Structures and Materials Panel Working Group 26 on High temperature cyclic behaviour of aerospace materials: Room temperature validation tests of Ti-6AI-4V. Neuilly sur Seine: Agard, 1994.
E, Smith James. High temperature furnace modeling and performance verifications: Final report, NAG8-708-final. Huntsville, Ala: Dept. of Chemical and Materials Engineering, College of Engineering, University of Alabama in Huntsville, 1992.
undifferentiated, J. H. Miller. Use of high-T[subscript c] superconducting magnetic sensors for nondestructive evaluation of subsurface defects: Final report. [Washington, DC: National Aeronautics and Space Administration, 1998.
Perdomo, Andrés Bertrand. Absorption of water and lubricating oils into porous nylon. El Segundo, Calif: The Aerospace Corporation, 1995.
Whittenberger, J. Daniel. Elevated temperature creep properties of NiAl cryomilled with and without Y₂O₃. [Washington, D.C: National Aeronautics and Space Administration, 1995.
E, Smith James. High temperature furnace modeling and performance verifications: Semi-annual progress report, NAG8-708-1. Huntsville, Ala: Dept. of Mechanical Engineering, College of Engineering, University of Alabama in Huntsville, 1988.
Hendricks, Robert C. Brush seal performance and durability issues based on T-700 engine test results. [Washington, DC]: National Aeronautics and Space Administration, 1994.
DeAngelis, V. Michael. Techniques for hot structures testing. Edwards, Calif: NASA Ames Research Center, Dryden Flight Research Facility, 1990.
DeAngelis, V. Michael. Techniques for hot structures testing. Edwards, Calif: NASA Ames Research Center, Dryden Flight Research Facility, 1990.
Reardon, Lawrence R. Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Reardon, Lawrence R. Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
MacConochie, Ian O. Design, fabrication, and tests of a metallic shell tile thermal protection system for space transportation. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Liebert, Curt H. Heat flux measurement in SSME turbine blade tester. [Washington, DC]: National Aeronautics and Space Administration, 1990.
Bizon, Peter T. Thermal-fatigue and oxidation resistance of cobalt-modified Udimet 700 alloy. Cleveland, Ohio: Lewis Research Center, 1986.
Hall, A. M. Summary report on elevated temperature tests for asbestos-free gasket materials. [Houston? Tex.]: National Association of Corrosion Engineers, 1990.
Center, Lewis Research, and United States. National Aeronautics and Space Administration., eds. High temperature mechanical characterization of ceramic matrix composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
High temperature strain gage technology for gas turbine engines. [Washington, DC: National Aeronautics and Space Administration, 1994.
Structural Testing Technology at High Temperature. Society for Experimental, 1991.
T, Lansaw P., Aerojet TechSystems Company (U.S.), and Lewis Research Center, eds. High-temperature, oxidation-rersistant thruster research. Sacramento, Calif: Aerojet Propulsion Division, Research & Technology, 1990.
T, Lansaw P., Aerojet TechSystems Company (U.S.), and Lewis Research Center, eds. High-temperature, oxidation-rersistant thruster research. Sacramento, Calif: Aerojet Propulsion Division, Research & Technology, 1990.
T, Lansaw P., Aerojet TechSystems Company (U.S.), and Lewis Research Center, eds. High-temperature, oxidation-rersistant thruster research. Sacramento, Calif: Aerojet Propulsion Division, Research & Technology, 1990.
A new test machine for measuring friction and wear in controlled atmospheres to 1200 ⁰C. [Washington, D.C.]: NASA, 1990.
United States. National Aeronautics and Space Administration., ed. High-temperature test facility at the NASA Lewis Engine Components Research Laboratory. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.
United States. National Aeronautics and Space Administration., ed. High-temperature test facility at the NASA Lewis Engine Components Research Laboratory. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.
United States. National Aeronautics and Space Administration., ed. High-temperature test facility at the NASA Lewis Engine Components Research Laboratory. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.
P, Desmond D., ed. High-temperature cyanide leaching of platinum-group metals from automobile catalysts--laboratory tests. Washington, D.C: U.S. Dept. of the Interior, Bureau of Mines, 1991.
P, Desmond D., ed. High-temperature cyanide leaching of platinum-group metals from automobile catalysts--laboratory tests. Washington, DC: U.S. Dept. of the Interior, 1991.
United States. National Aeronautics and Space Administration., ed. A high temperature testing system for ceramic composites: Final report. [Washington, D.C: National Aeronautics and Space Administration, 1994.
United States. National Aeronautics and Space Administration., ed. A high temperature testing system for ceramic composites: Final report. [Washington, D.C: National Aeronautics and Space Administration, 1994.
S, Mason Lee, Strumpf Hal J, and United States. National Aeronautics and Space Administration., eds. High-flux, high-temperature thermal vacuum qualification testing of a solar receiver aperature shield. [Washington, DC]: National Aeronautics and Space Administration, 1997.
S, Mason Lee, Strumpf Hal J, and United States. National Aeronautics and Space Administration., eds. High-flux, high-temperature thermal vacuum qualification testing of a solar receiver aperature shield. [Washington, DC]: National Aeronautics and Space Administration, 1997.
S, Mason Lee, Strumpf Hal J, and United States. National Aeronautics and Space Administration., eds. High-flux, high-temperature thermal vacuum qualification testing of a solar receiver aperature shield. [Washington, DC]: National Aeronautics and Space Administration, 1997.
S, Mason Lee, Strumpf Hal J, and United States. National Aeronautics and Space Administration., eds. High-flux, high-temperature thermal vacuum qualification testing of a solar receiver aperature shield. [Washington, DC]: National Aeronautics and Space Administration, 1997.
R, Bodis James, Bishop Chip, and United States. National Aeronautics and Space Administration., eds. Thermographic imaging for high-temperature composite materials: A defect detection study. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
R, Bodis James, Bishop Chip, and United States. National Aeronautics and Space Administration., eds. Thermographic imaging for high-temperature composite materials: A defect detection study. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Static tensile and tensile creep testing of five ceramic fibers at elevated temperatures: Final report. Laramie, Wyo: Composite Materials Research Group, Dept. of Mechanical Engineering, University of Wyoming, 1988.
1935-, Adams Donald Frederick, and United States. National Aeronautics and Space Administration., eds. Static tensile and tensile creep testing of five ceramic fibers at elevated temperatures. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.
Room temperature and elevated temperature composite sandwich joint testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
E, Sliney Harold, and Lewis Research Center, eds. Tribological properties of PM212: A high-temperature, self-lubricating, powder metallurgy composite. Cleveland, Ohio: Lewis Research Center, 1989.
Modification to the Langley 8-foot high temperature tunnel for hypersonic propulsion testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, ed. Nonlinear constitutive relations for high temperature application, 1984: Proceedings of a symposium held at NASA Lewis Research Center, Cleveland, Ohio, June 15-17, 1984. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1985.
Nonlinear constitutive relations for high temperature application, 1984: Proceedings of a symposium held at NASA Lewis Research Center, Cleveland, Ohio, June 15-17, 1984. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1985.
F, Adams Donald, Zimmerman Richard S, and Ames Research Center, eds. Static tensile and tensile creep testing of four boron nitride coated ceramic fibers at elevated temperatures: Final report. Moffett Field, Calif: NASA Ames Research Center, 1989.
Static tensile and tensile creep testing of four boron nitride coated ceramic fibers at elevated temperatures: Final report. Moffett Field, Calif: NASA Ames Research Center, 1989.
P, Bansal Narottam, Gyekenyesi John P, and NASA Glenn Research Center, eds. Dependency of shear strength on test rate in SiC/BSAS ceramic matrix composite at elevated temperature. [Cleveland, Ohio: NASA Glenn Research Center, 2003.
J, Skoch Gary, Wernet Judith H, and United States. National Aeronautics and Space Administration., eds. Demonstration of a stabilized alumina/ethanol colloidal dispersion technique for seeding high temperature air flows. [Washington, DC]: National Aeronautics and Space Administration, 1995.