Layerwise Theory for Dynamic Buckling and Postbuckling of Laminated Composite Cylindrical Shells
Author:
Affiliation:
1. Amirkabir University of Technology, Tehran 15914, Iran
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.281
Reference38 articles.
1. Thermal buckling of laminated composite shells
2. Thermal buckling of antisymmetric angle-ply laminated cylindrical shells
3. Large deflections of laminated cylindrical and doubly-curved panels under thermal loading
4. Shear deformable theories for cylindrical laminates - Equilibrium and buckling with applications
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