Effects of thickness and ply orientation on buckling of laminated plates
By: Dawn C. Jegley.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 87691.
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1986
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Composite materials -- Delamination.; Plates (Engineering); Buckling.; Laminates.; Loads (forces); Ply orientation.
Notes: Also available via Internet from the NTRS web site. Address as of 8/28/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860012146%5F1986012146.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1986. 1 microfiche.