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On the validity of Elber's results on fatigue crack closure for 2024-T3 aluminum

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References

  1. W. Elber, Damage Tolerance in Aircraft Structures, STP 486, American Society for Testing and Materials, Philadelphia (1971) 230–242.

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  2. T. T. Shih and R. P. Wei, Engineering Fracture Mechanics 6 (1974) 19–32.

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  3. T. C. Lindley and C. E. Richards, Materials Science and Engineering 14 (1974) 281–293.

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  4. E. F. J. Von Euw, R. W. Hertzberg, and R. Roberts, Stress Analysis and Growth of Cracks, STP 513, American Society for Testing and Materials, Philadelphia (1972) 230–259.

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  5. J. Vázquez, H. Ernst, and M. P. Gómez, Technical Note SIID, ITN-NT 2/75, R & D Service of the Argentine Navy (1975).

  6. R. A. Schmidt, Ph.D. Thesis, Lehigh University (1972).

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Authors and Affiliations

  1. Institute of Naval Technology, R. & D Service of the Argentine Navy, Estados Unidos 25, Buenos Aires, Argentina

    M. P. Gómez, H. Ernst & J. Vázquez

Authors
  1. M. P. Gómez
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  2. H. Ernst
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  3. J. Vázquez
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Gómez, M.P., Ernst, H. & Vázquez, J. On the validity of Elber's results on fatigue crack closure for 2024-T3 aluminum. Int J Fract 12, 178–180 (1976). https://doi.org/10.1007/BF00036027

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  • DOI: https://doi.org/10.1007/BF00036027

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