Postbuckling of long orthotropic plates under combined loading
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9076
Reference9 articles.
1. Postbuckling of orthotropic composite plates loaded in compression
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1. Post-buckling behavior of imperfect laminated composite plates with rotationally-restrained edges;Composite Structures;2015-07
2. Post-buckling analysis of composite plates under combined compression and shear loading using finite strip method;Finite Elements in Analysis and Design;2014-06
3. Boundary element modelling of non-linear buckling for symmetrically laminated plates;Mesh Reduction Methods;2009-08-27
4. Introducing a discrete modelling technique for buckling of panels under combined loading;Structural and Multidisciplinary Optimization;2007-11-01
5. A Boundary Element Approach to Buckling of Laminated Plates Subjected to Arbitrary In-Plane Loading;43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2002-04-22
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