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Review of fatigue-crack-growth prediction methods

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References

  1. Elber, W., in Damage Tolerance in Aircraft Structure, ASTM, 230–242 (1970).

  2. Newman, J.C., Jr., “Finite-Element Analysis of Fatigue Crack Propagation—Including the Effects of Crack Closure,”PhD Thesis, Virginia Polytechnic Institute and State University, Blacksburg, VA (May 1974).

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  3. Newman, J.C., Jr., “A Finite-Element Analysis of Fatigue Crack Closure,”Mechanics of Crack Growth, ASTM STP-590, ASTM, 281–301 (1976).

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References

  1. Hudson, C.M., “Effect of Stress Ratio on Fatigue Crack Growth in 7075-T6 and 2024-T3 Aluminum-Alloy Specimens,” NASA TN D-5390, NASA (Aug. 1969).

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Authors and Affiliations

  1. NASA Langley Research Center, 23665, Hampton, VA

    J. C. Newman Jr. (Research Engineer)

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  1. J. C. Newman Jr.
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Newman, J.C. Review of fatigue-crack-growth prediction methods. Experimental Mechanics 17, 399–400 (1977). https://doi.org/10.1007/BF02324208

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  • DOI: https://doi.org/10.1007/BF02324208

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