Analysis and Design for the Moderately Deep Postbuckling Behavior of Composite Plates
Author:
Affiliation:
1. Cardiff University, Cardiff, Wales CF24 3AA, United Kingdom
2. Indian Institute of Technology Hyderabad, Telangana 502 285, India
3. University of Bristol, Bristol, England BS8 1TR, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033875
Reference37 articles.
1. DicksonS. B.BiggersJ. N. “Postop: Postbuckled Open-Stiffener Optimum Panels—Theory and Capability,” NASA Rept. CR-172259, Jan. 1984, pp. 1–39.
2. Minimum Weight Design of Laminated Composite Plates for Postbuckling Performance
3. Optimization of composite, stiffened, imperfect panels under combined loads for service in the postbuckling regime
4. Multiobjective optimization of laminated plates for maximum prebuckling, buckling and postbuckling strength using continuous and discrete ply angles
5. MINIMUM-WEIGHT DESIGN OF COMPRESSIVELY LOADED STIFFENED PANELS FOR POSTBUCKLING RESPONSE
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