Research Catalog

  • Development and comparison of advanced reduced-basis methods for the transient structural analysis of unconstrained structures [microform] / David M. McGowan, Susan W. Bostic, Charles J. Camarda.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993
  • Damage characteristics and residual strength of composite sandwaich panels impacted with and without compression loading [microform] / : presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, session no. 15-damage tolerance : Long Beach, California, April 20-23, 1998 / David M. McGowan and Damodar R. Ambur.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects [microform] / David M. McGowan.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999
  • Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets [microform] / David M. McGowan and Damodar R. Ambur.

    • Text
    • Hampton, Va. : Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS53733
  • Compression response of a sandwich fuselage keel panel with and without damage / David M. McGowan and Damodar R. Ambur.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 1997.
    • 1997-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS72357
  • Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets / David M. McGowan and Damodar R. Ambur.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 1997.
    • 1997-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS53733

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