Simply-Supported Saddle-Shaped Thick Symmetric Cross-Ply Panels: Full Surface-Parallel Boundary Constraints
Author:
Affiliation:
1. University of Utah, Salt Lake City, Utah 84112-0560
2. Gebze Technical University, 41400 Kocaeli, Turkey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054921
Reference11 articles.
1. Levy-Type Boundary Fourier Analysis of Thick Clamped Hyperbolic-Paraboloidal Cross-Ply Panels
2. Levy-Type Boundary Fourier Analysis of Thick Cross-Ply Panels with Negative Gaussian Curvature
3. Analysis of Simply-Supported Saddle-Shaped Symmetric Cross-Ply Panels with No Surface-Parallel Boundary Constraints
4. ReddyJ. N., Mechanics of Laminated Composite Plates and Shells, Theory and Practice, 2nd ed., CRC Press, Boca Raton, FL, 2004, pp. 671–724, Chap. X1.
5. Levy type Fourier analysis of thick cross-ply doubly curved panels
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1. Flattening Effect of Negative Gaussian Curvature on Simply Supported Thick Asymmetric Cross-Ply Panels in the Absence of Surface-Parallel Edge Restraints;Journal of Aerospace Engineering;2020-11
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