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1

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

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2

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

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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

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

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5

Åkesson, B. Fatigue life of riveted steel bridges. CRC Press/Balkema, 2010.

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6

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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7

Saunders, Sam C. Reliability, Life Testing and the Prediction of Service Lives. Springer New York, 2007. http://dx.doi.org/10.1007/978-0-387-48538-6.

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8

Zaretsky, Erwin V. Fatigue criterion to system design, life and reliability--a primer. National Aeronautics and Space Administration, 1992.

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9

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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10

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

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11

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

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12

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

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13

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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14

Fatigue life of riveted steel bridges. CRC Press/Balkema, 2010.

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15

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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16

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

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17

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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18

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

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19

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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20

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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21

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

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22

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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23

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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24

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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25

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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26

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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27

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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28

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

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29

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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30

Zaretsky, Erwin V. Comparison of life theories for rolling-element bearings. National Aeronautics and Space Administration, 1995.

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31

Zaretsky, Erwin V. Comparison of life theories for rolling-element bearings. National Aeronautics and Space Administration, 1995.

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32

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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33

Pecht, Michael. Life-cycle forecasting, mitigation assessment, and obsolescence strategies: A guide to the prediction and management of electronic parts obsolescence. CALCE EPSC Press, 2002.

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34

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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35

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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36

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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37

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

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38

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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39

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

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40

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

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41

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

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42

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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43

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

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44

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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45

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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46

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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47

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

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48

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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49

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

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50

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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