Books on the topic 'Fatigue life prediction'

Ellyin, Fernand. Fatigue damage, crack growth, and life prediction. London: Chapman & Hall, 1997.

Fatigue Damage, Crack Growth and Life Prediction. Dordrecht: Springer Netherlands, 1996.

Ellyin, Fernand. Fatigue Damage, Crack Growth and Life Prediction. Dordrecht: Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-009-1509-1.

(Firm), Knovel, ed. Fatigue life prediction of composites and composite structures. Oxford: Woodhead Publishing, 2010.

O'Brien, T. Kevin. Tension fatigue analysis and life prediction for composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Kousky, Todd R. Conventional and probabilistic fatigue life prediction methodologies relevant to the P-3C aircraft. Monterey, Calif: Naval Postgraduate School, 1997.

Jones, David J. Cyclic fatigue damage characteristics observed for simple loadings extended to multiaxial life prediction. Cleveland, Ohio: Lewis Research Center, 1988.

Cui, Weicheng, Xiaoping Huang, and Fang Wang. Towards a Unified Fatigue Life Prediction Method for Marine Structures. Berlin, Heidelberg: Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-642-41831-0.

Alfred, Buch. Improvement of fatigue life prediction accuracy for various realistic loading spectra by use of correction factors. Haifa, Israel: Technion-Israel Institute of Technology, Dept. of Aeronautical Engineering, 1985.

Lifetime prediction and constitutive modelling for creep fatigue interaction. Berlin: Borntraeger, 1996.

Alfred, Buch. Ratio of crack initiation life to total fatigue life and use of local strain approach for prediction of fatigue life. Haifa: Technion Israel Institute of Technology, Dept. of Aeronautical Engineering, 1988.

Kemna, John G. Aluminum 7075-T6 fatigue data generation and probabilistic life prediction formulation. Monterey, Calif: Naval Postgraduate School, 1998.

Buxton, D. Pitting and corrosion fatigue life prediction in steam turbine rotor steels. Manchester: UMIST, 1993.

Ibrahim, Guven, and Kilic Bahattin, eds. Fatigue life prediction of solder joints in electronic packages with ANSYS. Boston, Mass: Kluwer Academic Publishers, 2002.

Alfred, Buch. Prediction of constant-amplitude fatigue life to failure under pulsating-tension (R > 0) by use of the local-strain-approach. Haifa, Israel: Technion - Israel Institute of Technology, Faculty of Aerospace Engineering, 1991.

Alfred, Buch. Prediction of constant-amplitude fatigue life to failure under pulsating-tension by use of the local-strain-approach. Haifa: Technion Israel Institute of Technology, 1989.

Nelson, R. S. Creep fatigue life prediction for engine hot section materials(Isotropic): Final report. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Madenci, Erdogan. Fatigue Life Prediction of Solder Joints in Electronic Packages with Ansys®. Boston, MA: Springer US, 2003.

Madenci, Erdogan, Ibrahim Guven, and Bahattin Kilic. Fatigue Life Prediction of Solder Joints in Electronic Packages with Ansys®. Boston, MA: Springer US, 2003. http://dx.doi.org/10.1007/978-1-4615-0255-5.

Radhakrishnan, V. Application of an energy-based life prediction model to bithermal and thermomechanical fatigue. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Radhakrishnan, V. Application of an energy-based life prediction model to bithermal and thermomechanical fatigue. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Saltsman, James F. Life prediction of thermomechanical fatigue using total strain version of strainrange partitioning (SRP): A proposal. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Nelson, R. S. Creep fatigue life prediction for engine hot section materials (isotropic): Second interim report. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Pickard, A. C. The application of 3-dimensional finite element methods to fracture mechanics andfatigue life prediction. Warley: EMAS, 1986.

Alfred, Buch. Prediction of fatigue life of notched specimens under aircraft loading and importance of the relative method in the case of local strain approach. Haifa: Technion Israel Institute of Technology, Dept. of Aeronautical Engineering, 1986.

S, Goel V., and American Society for Metals, eds. Fatigue life: Analysis and prediction : proceedings of the fatigue program and related papers presented at the International Conference and Exposition on Fatigue, Corrosion Cracking, Fracture Mechanics and Failure Analysis, 2-6 December, 1985, Salt Lake City, Utah, USA. [Metals Park, OH]: ASM, 1986.

1932-, Zamrik S. Y., Halford Gary R, American Society of Mechanical Engineers. Pressure Vessels and Piping Division., and International Mechanical Engineering Congress and Exposition (1994 : Chicago, Ill.), eds. Material durability/life prediction modeling: Materials for the 21st century : presented at 1994 International Mechanical Engineering Congress and Exposition, Chicago, Illinois, November 6-11, 1994. New York: American Society of Mechanical Engineers, 1994.

Alfred, Buch. NSA and LSA predictions of the effect of reference stress, loading sequence, stress concentration and specimen material on fatigue life in the case of realistic loading spectra. Haifa, Israel: Technion Israel Institute of Technology, 1992.

R, Mohan, Lam Poh-Sang, American Society of Mechanical Engineers. Pressure Vessels and Piping Division., and Pressure Vessels and Piping Conference (2000 : Seattle, Wash.), eds. Understanding and predicting material degradation: Presented at the 2000 ASME Pressure Vessels and Piping Conference, Seattle, Washington, July 23-27, 2000. New York, N.Y: American Society of Mechanical Engineers, 2000.

Contact Fatigue: Life Prediction and Palliatives. Storming Media, 2002.

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.

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

S, Johnson W., and Hillberry B. M, eds. Probabilistic aspects of life prediction. W. Conshohocken, PA: ASTM International, 2004.

Fatigue Damage, Crack Growth and Life Prediction. Springer, 2011.

Vassilopoulos, Anastasios P. Fatigue Life Prediction of Composites and Composite Structures. Elsevier Science & Technology, 2019.

Vassilopoulos, Anastasios P. Fatigue Life Prediction of Composites and Composite Structures. Elsevier Science & Technology, 2019.

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

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.

National Aeronautics and Space Administration (NASA) Staff. Comparison of Fatigue Life Prediction Methodologies for Rotorcraft. Independently Published, 2018.

Vassilopoulos, Anastasios P. Fatigue life prediction of composites and composite structures. Woodhead Publishing Limited, 2010. http://dx.doi.org/10.1533/9781845699796.

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.

Fatigue Life Prediction of Composites and Composite Structures. Elsevier, 2020. http://dx.doi.org/10.1016/c2017-0-02509-0.

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.

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.

National Aeronautics and Space Administration (NASA) Staff. Advances in Fatigue Life Prediction Methodology for Metallic Materials. Independently Published, 2018.

Probabilistic Modeling and Simulation of Metal Fatigue Life Prediction. Storming Media, 2002.

R, Halford Gary, and United States. National Aeronautics and Space Administration., eds. Fatigue life prediction modeling for turbine hot section materials. [Washington, DC]: National Aeronautics and Space Administration, 1988.

United States. National Aeronautics and Space Administration., ed. Acoustic fatigue life prediction for nonlinear structures with multiple resonant modes: Final report. [Washington, DC: National Aeronautics and Space Administration, 1992.

United States. Army Aviation Research and Technology Activity. and Langley Research Center, eds. A comparison of fatigue life prediction methodologies for rotor craft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.