Analytical/Experimental Behavior of Anisotropic Rectangular Panels Under Linearly Varying Combined Loads
Author:
Affiliation:
1. Politecnico di Torino, 10129 Turin, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1398
Reference11 articles.
1. Nonlinear analysis of anisotropic plates with initial imperfections and various boundary conditions subjected to combined biaxial compression and shear loads
2. Elastic Stability of Simply Supported Flat Rectangular Plates Under Critical Combinations of Transverse Compression and Longitudinal Bending
3. Elastic Stability of Simply Supported Flat Rectangular Plates Under Critical Combinations of Longitudinal Bending, Longitudinal Compression, and Lateral Compression
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