Research Catalog

  • Computational simulation of damage progression of composite thin shells subjected to mechanical loads [microform] / P.K. Gotsis, C.C. Chamis, L. Minnetyan.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension [microform] / Marshall Rouse ... [et al.].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Influence of an asymmetric ring on the modeling of an orthogonally stiffened cylindrical shell [microform] / Naveen Rastogi and Eric R. Johnson.

    • Text
    • Blacksburg, Va. : Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60750
  • PRSEUS pressure cube test data and response / Andrew E. Lovejoy.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37999

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