Thermomechanical Postbuckling Response and First-Ply Failure Analysis of Doubly Curved Panels
Author:
Affiliation:
1. Indian Institute of Technology, Kharagpur 721 302, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.6849
Reference22 articles.
1. Thermal buckling of laminated composite shells
2. THERMOELASTIC BUCKLING OF THIN CYLINDRICAL SHELLS BASED ON IMPROVED STABILITY EQUATIONS
3. BUCKLING OF COMPOSITE CYLINDRICAL SHELLS UNDER MECHANICAL AND THERMAL LOADS
4. Refined theory for non-linear buckling of heated composite shallow spherical shells
5. Large deflections of laminated cylindrical and doubly-curved panels under thermal loading
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