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Postbuckling of orthotropic composite plates loaded in compressionThe nonlinear large deflection equations of von Karman are written for 'specially' orthotropic plates. The equations are then manipulated to determine the parameters required to establish postbuckling behavior. It is found that only two new parameters are needed beyond those required for buckling. By assuming trigonometric functions in one direction, the plate equations are converted into ordinary nonlinear differential equations which are solved numerically using a two point boundary problem solver that makes use of Newton's method. The postbuckling behavior is obtained for simply supported and clamped, long, rectangular, orthotropic plates covering the complete range of dimensions and material properties.
Document ID
19820046589
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Stein, M.
(NASA Langley Research Center Structures and Dynamics Div., Hampton, VA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 82-0778
Meeting Information
Meeting: In: Structures, Structural Dynamics and Materials Conference
Location: New Orleans, LA
Start Date: May 10, 1982
End Date: May 12, 1982
Accession Number
82A30124
Distribution Limits
Public
Copyright
Other

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