Books on the topic 'Methodology for evaluating the fatigue life'

Fatigue life and crack growth prediction methodology. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

P, Phillips E., Everett R. A, and Langley Research Center, eds. Fatigue life and crack growth prediction methodology. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

P, Phillips E., Swain M. H, and Langley Research Center, eds. Fatigue-life prediction methodology using small-crack theory. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Kevin, O'Brien T., Rousseau Carl Q, and United States. National Aeronautics and Space Administration., eds. Fatigue life methodology for tapered composite flexbeam laminates. [Washington, DC: National Aeronautics and Space Administration, 1997.

Kevin, O'Brien T., Rousseau Carl Q, and Langley Research Center, eds. Fatigue life methodology for tapered composite flexbeam laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

P, Phillips E., Swain M. H, and Langley Research Center, eds. Fatigue-life prediction methodology using small-crack theory. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Kevin, O'Brien T., Rousseau Carl Q, and Langley Research Center, eds. Fatigue life methodology for tapered composite flexbeam laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

P, Phillips E., Swain M. H, and Langley Research Center, eds. Fatigue-life prediction methodology using small-crack theory. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

P, Phillips E., Swain M. H, and Langley Research Center, eds. Fatigue-life prediction methodology using small-crack theory. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Kevin, O'Brien T., Rousseau Carl Q, and United States. National Aeronautics and Space Administration., eds. Fatigue life methodology for tapered composite flexbeam laminates. [Washington, DC: National Aeronautics and Space Administration, 1997.

Center, Langley Research, ed. Advances in fatigue life prediction methodology for metallic minerals. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Ronald, Krueger, and Langley Research Center, eds. Fatigue life methodology for bonded composite skin/stringer configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

Ronald, Krueger, and Langley Research Center, eds. Fatigue life methodology for bonded composite skin/stringer configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

D, Bartlett F., Elber Wolf, United States. Army Aviation Research and Technology Activity., and Langley Research Center, eds. Probabalistic fatigue methodology for six nines reliability. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

C, Chamis C., and Lewis Research Center, eds. A methodology for evaluating the reliability and risk of structures under complex service environments. [Cleveland, Ohio: NASA Lewis Research Center, 1990.

Development of a fatigue-life methodology for composite structures subjected to out-of-plane load components. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1991.

T, Kedward K., and Ames Research Center, eds. Development of a fatigue-life methodology for composite structures subjected to out-of-plane load components. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1991.

Development of a fatigue-life methodology for composite structures subjected to out-of-plane load components. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1991.

United States. National Aeronautics and Space Administration., ed. Profiled roller stress/fatigue life analysis methodology and establishment of an appropriate stress/life exponent: Results summary. [Washington, DC: National Aeronautics and Space Administration, 1997.

Korkmaz, Sinan. Uniform Material Law: Extension to High-Strength Steels: A Methodology to Predict Fatigue Life of High-Strength Steels. VDM Verlag Dr. Müller, 2010.

Modeling and life prediction methodology for titanium matrix composites subjected to mission profiles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Modeling and life prediction methodology for titanium matrix composites subjected to mission profiles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

R, Mohan, Mehta H. S, American Society of Mechanical Engineers. Pressure Vessels and Piping Division., and ASME Pressure Vessels and Piping Conference (1999 : Boston, Massachusetts), eds. Advances in life prediction methodology: Presented at the 1999 ASME Pressure Vessels and Piping Conference : Boston, Massachusetts, August 1-5, 1999. New York, N.Y: American Society of Mechanical Engineers, 1999.

Mohan, Raj. Advances in Life Prediction Methodology: 1999 Asme Pressure Vessels and Piping Conference, Boston, Massachusetts, August 1-5, 1999 (P V P). Amer Society of Mechanical, 1999.