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  • Response of composite materials to low velocity impact [microform] / K. Srinivasan, W.C. Jackson and J.A. Hinkley.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [St. Louis, Mo.] : US Army Aviation Systems Command, Aviation R&T Activity ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Damage tolerance in filament-wound graphite/epoxy pressure vessels [microform] : final report / William E. Simon, principal investigator, Vinh D. Nguyen, research associate, Ravi K. Chenna, research assistant.

    • Text
    • Beaumont, Tex. : Lamar University, College of Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Evaluation of the impact response of textile composites [microform] / M.A. Portanova.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Probabilistic evaluation of blade impact damage [microform] / C.C. Chamis, G.H. Abumeri.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS51549

  • Design and testing of an energy-absorbing crewseat for the F/FB-111 aircraft [microform] : volume II, data from seat testing / S. Joseph Shane.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
    • 1985

  • Concepts for improving the damage tolerance of composite compression panels [microform] / Marvin D. Rhodes, Jerry G. Williams.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS95389

  • Effect of impact damage and open holes on the compression strength of tough resin/high strain fiber laminates [microform] / Jerry G. Williams.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS95394

  • Impacts of space shuttle thermal protection system tile on an F-15 aircraft vertical tail [microform] / William L. Ko.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, [1985]
    • 1985

  • Fuel containment, lightning protection, and damage tolerance in large composite primary aircraft structures [microform] / Charles F. Griffin and Arthur M. James.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985

  • Probabilistic evaluation of blade impact damage / C.C. Chamis, G.H. Abumeri.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2003.
    • 2003-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS51549

  • Normalization of impact energy by laminate thickness for compression after impact testing / A.T. Nettles and S.M. Hromisin.

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37983

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