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Buckling analysis of fully anisotropic plates containing cutouts and elastically restrained edgesAn analysis is developed which combines the Ritz and collocation methods for the stability solution of an anisotropic plate with a cutout and elastically restrained edges. Results are presented which agree closely with experiment for isotropic and orthotropic materials. Results are also given for restrained anisotropic plates with circular holes loaded in compression and shear. Difference is noted in the critical buckling loads between displacement and stress loaded panels as hole size is increased. Clamping is also seen to affect the trends in buckling associated with hole size.
Document ID
19920051674
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jones, Kevin M.
(NASA Langley Research Center Hampton, VA, United States)
Klang, Eric C.
(North Carolina State University Raleigh, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 92-2279
Meeting Information
Meeting: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Dallas, TX
Country: United States
Start Date: April 13, 1992
End Date: April 15, 1992
Accession Number
92A34298
Funding Number(s)
CONTRACT_GRANT: NAG1-917
Distribution Limits
Public
Copyright
Other

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