Books on the topic 'Fatigue life of metals'

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1

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

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2

Naman, Recho, ed. Fatigue life analyses of welded structures. London: ISTE, 2006.

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3

Cyclic plasticity and low cycle fatigue life of metals. Amsterdam: Elsevier, 1991.

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4

Zaretsky, Erwin V. Selection [of] rolling-element bearing steels for long-life application. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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5

Zaretsky, Erwin V. Selection [of] rolling-element bearing steels for long-life application. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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6

Zaretsky, Erwin V. Selection [of] rolling-element bearing steels for long-life application. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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7

Zaretsky, Erwin V. Selection [of] rolling-element bearing steels for long-life application. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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8

Halford, Gary R. Stirling engine -- available tools for long-life assessment. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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9

Farahmand, Bahram. Fatigue and fracture mechanics of high risk parts: Application of LEFM & FMDM theory. New York: Chapman & Hall, 1997.

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10

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.

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11

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.

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12

Farahmand, Bahram. Fatigue and fracture mechanics of high risk parts: Application of LEFM & FMDM theory. Dordrecht: Springer, 1997.

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13

Majumdar, Bhaskar S. Isothermal fatigue mechanisms in Ti-based metal matrix composites [microform]. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1993.

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14

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

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15

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

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16

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

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17

Finney, J. M. Cold expansion and interference for extending the fatigue life of multi-layer metal joints. Melbourne, Australia: Aeronautical Research Laboratory, 1993.

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18

Zaretsky, Erwin V. Comparison of life theories for rolling-element bearings. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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19

Zaretsky, Erwin V. Comparison of life theories for rolling-element bearings. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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20

Johnson, W. S. Fatigue damage growth mechanisms in continuous fiber reinforced titanium matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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21

Johnson, W. S. Fatigue damage growth mechanisms in continuous fiber reinforced titanium matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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22

Castelli, Michael G. Isothermal damage and fatigue behavior and SCS-6/timetal 21S [0/90]s composite at 650C̊. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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23

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

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24

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

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25

ASME International Gas Turbine and Aeroengine Congress and Exposition (33rd 1988 Amsterdam, Netherlands). Toward improved durability in advanced aircraft engine hot sections: Presented at the 1988 ASME Turbo Expo - Land, Sea & Air, the 33rd ASME International Gas Turbine and Aeroengine Congress and Exposition, Amsterdam, the Netherlands, June 5-9, 1988 : sponsored by the Aircraft Committee, ASME International Gas Turbine Institute. New York: American Society of Mechanical Engineers, 1988.

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26

1935-, Marsh K. J., and Pook L. P, eds. Metal fatigue. Mineola, NY: Dover Publications, 1999.

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27

Cardona, D. C. Fatigue of brittle metals. Birmingham: University of Birmingham, 1990.

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28

1954-, Hejwowski Tadeusz, ed. Thermal fatigue of metals. New York: M. Dekker, 1991.

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29

Schijve, Jaap. Biaxial Fatigue of Metals. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-23606-3.

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30

Bathias, Claude. Fatigue Limit in Metals. Hoboken, USA: John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118648704.

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31

Correia, José A. F. O., Abílio M. P. De Jesus, António Augusto Fernandes, and Rui Calçada, eds. Mechanical Fatigue of Metals. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-13980-3.

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32

V, Bicego, Nitta A, Viswanathan Ramaswamy, Comité de Informática do Setor de Energia Elétrica., and Gruppo italiano frattura, eds. Materials ageing and component life extension. Warley: Engineering Materials Advisory Services, 1995.

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33

Milella, P. P. Fatigue and corrosion in metals. Milan: Springer, 2013.

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34

Milella, Pietro Paolo. Fatigue and Corrosion in Metals. Milano: Springer Milan, 2013. http://dx.doi.org/10.1007/978-88-470-2336-9.

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35

Milella, Pietro Paolo. Fatigue and Corrosion in Metals. Milano: Springer Milan, 2013.

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36

United States. National Aeronautics and Space Administration, ed. Fatigue life of laser cut metals. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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37

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

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38

Cho, Naman, Tom Lassen, and Naman Recho. Fatigue Life Analyses of Welded Structures. Wiley & Sons, Incorporated, John, 2010.

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39

Center, Langley Research, ed. Corrosion fatigue crack propagation in metals. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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40

Polák, J. Cyclic plasticity and low cycle fatigue life of metals. Elsevier, 1991.

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41

Lassen, Tom, and Naman Récho. Fatigue Life Analyses of Welded Structures: Flaws. Wiley & Sons, Incorporated, John, 2013.

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42

Lassen, Tom, and Naman Récho. Fatigue Life Analyses of Welded Structures: Flaws. Wiley & Sons, Incorporated, John, 2013.

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43

Lassen, Tom, and Naman Récho. Fatigue Life Analyses of Welded Structures: Flaws. Wiley & Sons, Incorporated, John, 2010.

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44

Lassen, Tom, Naman Récho, and Naman Récho. Fatigue Life Analyses of Welded Structures: Flaws. Wiley & Sons, Incorporated, John, 2010.

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45

A, Lerch Bradley, Saltsman James F, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Proposed framework for thermomechanical life modeling of metal matrix composites. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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46

Isothermal life prediction of composite lamina using a damage mechanics approach. [Washington, DC]: National Aeronautics and Space Administration, 1989.

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47

J, Herrmann D., Hillberry B. M, and Langley Research Center, eds. Fatigue-life behavior and matrix fatigue crack spacing in unnotched SCS-6/Timetal℗ʾ 21A metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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48

J, Herrmann D., Hillberry B. M, and Langley Research Center, eds. Fatigue-life behavior and matrix fatigue crack spacing in unnotched SCS-6/Timetal® 21A metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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49

J, Herrmann D., Hillberry B. M, and Langley Research Center, eds. Fatigue-life behavior and matrix fatigue crack spacing in unnotched SCS-6/Timetal® 21A metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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50

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

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