Last edited by Megor
Tuesday, April 28, 2020 | History

3 edition of The NASA monographs on shell stability design recommendations found in the catalog.

The NASA monographs on shell stability design recommendations

The NASA monographs on shell stability design recommendations

a review and suggested improvements

by

  • 63 Want to read
  • 7 Currently reading

Published by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor in Hampton, Va, Springfield, VA .
Written in English

    Subjects:
  • Design analysis.,
  • Thin walled shells.

  • Edition Notes

    StatementMichael P. Nemeth and James H. Starnes, Jr.
    Series[NASA technical paper] -- NASA/TP-1998-206290., NASA technical paper -- 206290.
    ContributionsStarnes, James H., Langley Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL15548778M

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The NASA monographs on shell stability design recommendations Download PDF EPUB FB2

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The layup of the classical CFRP shell is [±45°/0°/90° ] s which leads to a constant stiffness. The second shell is a variable angle tow CFRP shell with a layup of [±45°/±φ°(x)] s, x being the shell axial coordinate, where ±φ(x) is a steered ply with constant route has the following values: φ(0) = 60°, φ(L/2) = 15° and φ(L) = −60°, with L being the length of the by: 5.

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