Improvements to a method for the geometrically nonlinear analysis of compressively loaded stiffened composite panels [microform] : progress report for the period July 1991 to December 1991.

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Bibliographic Details
Corporate Author:	United States. National Aeronautics and Space Administration
Format:	Government Document Microfilm Book
Language:	English
Published:	[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Center, distributor], [1991]
Series:	NASA contractor report ; NASA CR-192183.
Subjects:	Compression loads. Nonlinearity. Rigid structures. Stiffness matrix. Strain distribution. Structural analysis.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.26:192183
NAS 1.26:192183	Restricted Place a Hold