Books on the topic 'Elevated temperature fatigue'

Orange, Thomas W. Elevated temperature crack propogation. [Washington, DC: National Aeronautics and Space Administration, 1993.

Orange, Thomas W. Elevated temperature crack propagation. [Washington, DC: National Aeronautics and Space Administration, 1993.

Healy, Joseph Cornelius. Short fatigue crack growth at elevated temperature. Birmingham: Universityof Birmingham, 1989.

Piascik, RS, RP Gangloff, and A. Saxena, eds. Elevated Temperature Effects on Fatigue and Fracture. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 1997. http://dx.doi.org/10.1520/stp1297-eb.

Leeuwen, H. P. van. Automated measurement of crack length and load line displacement at elevated temperature. Neuilly sur Seine, France: AGARD, 1988.

Hodkinson, Victoria. The effect of waveshape on fatigue crack growth in nickel superalloys at elevated temperature. Portsmouth: University of Portsmouth, Dept. of Mechanical and Manufacturing Engineering, 1997.

Antunes, Fernando Jorge Ventura. Influence of frequency, stress ratio and stress state on fatigue crack growth in nickel base superalloys at elevated temperature. Portsmouth: University of Portsmouth, Dept. of Mechanical and Manufacturing Engineering, 1999.

C, Becht, American Society of Mechanical Engineers., and Nihon Kikai Gakkai, eds. Structural design for elevated temperature environments -- creep, ratchet, fatigue, and fracture: Presented at the 1989 ASME Pressure Vessels and Piping Conference, JSME co-sponsorship, Honolulu, Hawaii, July 23-27, 1989. New York, N.Y. (345 E. 47th St., New York 10017): American Society of Mechanical Engineers, 1989.

Montesano, John. Fatigue of polymer matrix composites at elevated temperatures. New York: Nova Science Publishers, 2011.

Montesano, John, and John Montesano. Fatigue of polymer matrix composites at elevated temperatures. New York: Nova Science Publishers, 2011.

Ellis, J. R. Results of an interlaboratory fatigue test program conducted on Alloy 800H at room and elevated temperatures. [Washington, D.C.]: National Aeronautics and Space Administration, 1985.

Couch, Peter David. Fatigue and fracture of an Aluminium Lithium based metal matrix composite at both ambient and elevated temperatures. Birmingham: University of Birmingham, 1994.

Dalby, Sara. The effects of frequency and waveshape on the fatigue crack growth of an advanced nickel base superalloy at elevated temperatures. Portsmouth: University of Portsmouth, Dept. of Mechanical and Manufacturing Engineering, 2002.

United States. National Aeronautics and Space Administration, ed. Elevated temperature biaxial fatigue. [Washington, DC]: National Aeronautics and Space Administration, 1985.

Elevated temperature biaxial fatigue. [Washington, DC]: National Aeronautics and Space Administration, 1985.

Elevated temperature effects on fatigue and fracture. West Conshohocken, PA: ASTM, 1997.

H, Van Stone R., and United States. National Aeronautics and Space Administration., eds. Elevated temperature crack growth: Final report. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Room temperature and elevated temperature composite sandwich joint testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Sreeramesh, Kalluri, United States. Army Aviation Research and Technology Activity., and United States. National Aeronautics and Space Administration., eds. Elevated temperature axial and torsional fatigue behavior of Haynes 188. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Elevated temperature axial and torsional fatigue behavior of Haynes 188. [Washington, DC: National Aeronautics and Space Administration, 1995.

Fretting Fatigue Behavior of a Titanium Alloy Ti-6AL-4V at Elevated Temperature. Storming Media, 2002.

Residual Strength After Fatigue of a Cross-Ply Metal Matrix Composite at Elevated Temperature. Storming Media, 1997.

John, Gayda, and United States. National Aeronautics and Space Administration., eds. An overview of elevated temperature damage mechanisms and fatigue behavior of a unidirectional SCS-6/Ti-15-3 composite. [Washington, DC: National Aeronautics and Space Administration, 1993.

Residual Strength after Fatigue of Unidirectional and Cross-Ply Metal Matrix Composites at Elevated Temperature. Storming Media, 1996.

Monotonic, Creep-Rupture, and Fatigue Behavior of Carbon Fiber Reinforced Silicon Carbide (C/SiC) at an Elevated Temperature. Storming Media, 2004.

A study of elevated temperature testing techniques for the fatigue behavior of PMCS: Application to T650-35/AMB21. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Elevated temperature crack growth: Presented at the Winter Annual Meeting of the American Society of Mechanical Engineers, Dallas, Texas, November 25-30, 1990. New York, N.Y: The Society, 1990.

Fiber Volume Fraction Effects on Fatigue Response of a SCS-6/Ti-15-3 Metal Matrix Composite at Elevated Temperature. Storming Media, 1997.

Center, Langley Research, ed. Effects of moisture, elevated temperature, and fatigue loading on the behavior of graphite/epoxy buffer strip panels with center cracks. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

United States. National Aeronautics and Space Administration., ed. Fatigue life prediction of an intermetallic matrix composite at elevated temperatures. [Washington, DC]: National Aeronautics and Space Administration, 1991.

Yoshiki, Oshida, and United States. National Aeronautics and Space Administration, eds. Grain boundary oxidation and fatigue crack growth at elevated temperatures. [Washington, DC: National Aeronautics and Space Administration, 1986.

Miller, Brett A., Roch J. Shipley, Ronald J. Parrington, and Daniel P. Dennies, eds. Analysis and Prevention of Component and Equipment Failures. ASM International, 2021. http://dx.doi.org/10.31399/asm.hb.v11a.9781627083294.

United States. National Aeronautics and Space Administration., ed. The analysis of fatigue crack growth mechanism and oxidation and fatigue life at elevated temperatures. [Washington, DC: National Aeronautics and Space Administration, 1988.

P, Gyekenyesi J., and United States. National Aeronautics and Space Administration., eds. Reliability and life prediction of ceramic composite structures at elevated temperatures. [Washington, DC: National Aeronautics and Space Administration, 1994.

Reliability and life prediction of ceramic composite structures at elevated temperatures. [Washington, DC: National Aeronautics and Space Administration, 1994.

(Editor), S. Mall, and A. Nagar (Editor), eds. Fatigue and Fracture at Elevated Temperatures: Presented at the 1995 Asme International Mechanical Engineering Congress and Exposition, November 12-17 (Ad). American Society of Mechanical Engineers, 1995.

Monotonic and Fatigue Behavior of 2-D Woven Ceramic Matrix Composite at Room and Elevated Temperatures (Blackglas/Nextel 312). Storming Media, 1998.

Arvind, Nagar, Mall S, American Society of Mechanical Engineers. Aerospace Division., and International Mechanical Engineering Congress and Exposition (1995 : San Francisco, Calif.), eds. Fatigue and fracture at elevated temperatures: Presented at the 1995 ASME International Mechanical Engineering Congress and Exposition, November 12-17, 1995, San Francisco, California. New York, N.Y: American Society of Mechanical Engineers, 1995.