Last edited by Shajora
Saturday, May 2, 2020 | History

2 edition of Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels found in the catalog.

Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels

William L. Ko

Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels

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  • 29 Currently reading

Published by National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, National Technical Information Service, distributor] in [Washington, DC], [Springfield, Va .
Written in English

    Subjects:
  • Aircraft structures.,
  • Aspect ratio.,
  • Buckling.,
  • Combined stress.,
  • Compressive strength.,
  • Honeycomb cores.,
  • Hypersonic vehicles.,
  • Panels.,
  • Rayleigh-Ritz method.,
  • Sandwich structures.,
  • Shear strength.,
  • Structural analysis.

  • Edition Notes

    StatementWilliam L. Ko and Raymond H. Jackson.
    SeriesNASA technical memorandum -- 4290.
    ContributionsJackson, Raymond H., United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL15406122M


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Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels by William L. Ko Download PDF EPUB FB2