Buckling behavior of long symmetrically laminated plates subjected to shear and linearly varying axial edge loads

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National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor , Hampton, Va, [Springfield, Va
Anisotropy., Anisotropic plates., Buckling., Axial loads., Graphite-epoxy composites., Plates (Structural members), Lamin
StatementMichael P. Nemeth.
SeriesNASA technical paper -- 3659.
ContributionsLangley Research Center.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL15496298M

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