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  • Strain energy release rate as a function of temperature and preloading history utilizing the edge delamination fatigue test method [microform]/ Richard S. Zimmerman and Donald F. Adams.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Combined effect of matrix cracking and stress-free edge on delamination [microform] / S.A. Salpekar and T.K. O'Brien.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [ St. Louis, MO] : US Army Aviation Systems Command, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67326

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