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  • Buckling and damage resistance of transversely-loaded composite shells [microform] / by Brian L. Wardle.

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

  • Buckling analysis for stiffened anisotropic circular cylinders based on Sanders' nonlinear shell theory / Michael P. Nemeth.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2014.
    • 2014-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55308

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