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Loads and Deformations of Buckled Rectangular PlatesThe nonlinear large-deflection equations of von Karman for plates are converted into a set of linear equations by expanding the displacements Into a power series in terms of an arbitrary parameter. The postbuckling behavior of simply supported rectangular plates subjected to longitudinal compression and subject to a uniform temperature rise is investigated in detail by solving the first few of the equations. Experimental data are presented for the compression problem. Comparisons are made for total shortening and local strains and deflections which indicate good agreement between experimental and theoretical results.
Document ID
19980235521
Acquisition Source
Langley Research Center
Document Type
Thesis/Dissertation
Authors
Stein, Manuel
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 18, 2013
Publication Date
January 1, 1959
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TR-R-40
Report Number: NASA-TR-R-40
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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