Bilevel Optimization and Postbuckling of Highly Strained Composite Stiffened Panels
Author:
Affiliation:
1. University of Bath, BA2 7AY Bath, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.22206
Reference16 articles.
1. Buckling of Unidirectionally Loaded Composite Plates with One Free and One Rotationally Restrained Unloaded Edge
2. Simultaneous cost and weight minimization of composite-stiffened panels under compression and shear
3. Optimum design using viconopt, a buckling and strength constraint program for prismatic assemblies of anisotropic plates
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