Buckling behavior of long symmetrically laminated plates subjected to shear and linearly varying axial edge loads
By: Michael P. Nemeth.
Contributors: Langley Research Center.
Series: NASA technical paper -- 3659.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1997
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Anisotropy.; Anisotropic plates.; Buckling.; Axial loads.; Graphite-epoxy composites.; Plates (Structural members); Laminates.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 98-0733-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.