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1

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

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2

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

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3

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

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4

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

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5

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

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6

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

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7

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

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8

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

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9

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

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10

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

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11

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

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12

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

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13

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

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14

Yamada, Kentaro. Fatigue life prediction of welded joints using fracture mechanics. Afdelingen for bærende konstruktioner, Danmarks tekniske højskole, 1990.

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15

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

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16

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

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17

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

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18

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

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19

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

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20

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

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21

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

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22

Center, Lewis Research, ed. Isothermal fatigue, damage accumulation, and life prediction of a woven PMC. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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23

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

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24

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

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25

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

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26

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

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27

Sang-Shik, Kim, and Langley Research Center, eds. Environment enhanced fatigue crack propagation in metals: Inputs to fracture mechanics life prediction models. National Aeronautics and Space Administration, Langley Research Center, 1993.

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28

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

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29

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

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30

Sreeramesh, Kalluri, Halford Gary R, and United States. National Aeronautics and Space Administration., eds. Application of an energy-based life prediction model to bithermal and thermomechanical fatigue. National Aeronautics and Space Administration, 1994.

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31

Sreeramesh, Kalluri, Halford Gary R, and United States. National Aeronautics and Space Administration., eds. Application of an energy-based life prediction model to bithermal and thermomechanical fatigue. National Aeronautics and Space Administration, 1994.

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32

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

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33

V, Poplawski J., Miller C. R, and NASA Glenn Research Center, eds. Rolling bearing life prediction-past, present, and future. National Aeronautics and Space Administration, Glenn Research Center, 2000.

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34

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

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35

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

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36

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

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37

F, Schoendorf J., Lin L. S, and United States. National Aeronautics and Space Administration, eds. Creep fatigue life prediction for engine hot section materials (isotropic): Interim report. National Aeronautics and Space Administration, Lewis Research Center, 1986.

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38

J, Verilli Michael, Halford G. R, and United States. National Aeronautics and Space Administration., eds. A creep cavity growth model for creep-fatigue life prediction of a unidirectional W/Cu composite. National Aeronautics and Space Administration, 1992.

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39

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

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40

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. National Aeronautics and Space Administration, Langley Research Center, 1990.

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41

Klevtsov, Ivan. Strained condition diagnosis and fatigue life prediction for metals under cyclic temperature oscillations. Tallinn Technical University, 1994.

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42

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

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43

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

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44

United States. National Aeronautics and Space Administration., ed. Fatigue behavior and life prediction of a SiC/Ti-24Al-11Nb composite under isothermal conditions. NASA, 1991.

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45

Center, Langley Research, ed. Empirical modeling of environment-enhanced fatigue crack propagation in structural alloys for component life prediction. National Aeronautics and Space Administration, Langley Research Center, 1995.

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46

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. Technion Israel Institute of Technology, Dept. of Aeronautical Engineering, 1986.

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47

Adam, Pintz, and United States. National Aeronautics and Space Administration., eds. Ceramic material life prediction: A program to translate ANSYS results to CARES/LIFE reliability analysis : final report. National Aeronautics and Space Administration, 1994.

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48

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

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49

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. American Society of Mechanical Engineers, 1999.

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50

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. ASM, 1986.

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