Research Catalog

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  • Influence of impactor mass on the damage characteristics and failure strength of laminated composite plates [microform] : presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference : Long Beach, California, April 20-23, 1998 / Damodar R. Ambur and Heather L. Kemmerly.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Orbital impacts and the space shuttle windshield [microform] / Karen S. Edelstein.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Effects of through-the-thickness stitching on impact and interlaminar fracture properties of textile graphite/epoxy laminates [microform] / Suresh K. Sharma and Bhavani V. Sankar.

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

  • The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy [microform] / Alan T. Nettles.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Modeling of high-strain-rate deformation, fracture, and impact behavior of advanced gas turbine engine materials at low and elevated temperatures [microform] / Mostafa Shazly, David Nathenson, and Vikas Prakash.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55231

  • Instrumented impact and residual tensile strength testing of eight-ply carbon/epoxy specimens [microform] / A.T. Nettles.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, VA : For sale by the National Technical Information Service], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68606

  • A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications / A.T. Nettles.

    • Text
    • Huntsville, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24323

  • 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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