Framework for the Buckling Optimization of Variable-Angle Tow Composite Plates
Author:
Affiliation:
1. Department of Aerospace Engineering, 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.J054029
Reference37 articles.
1. Variable stiffness composite panels: Effects of stiffness variation on the in-plane and buckling response
2. Buckling analysis and optimisation of variable angle tow composite plates
3. Postbuckling optimisation of variable angle tow composite plates
4. Optimization of Variable-Stiffness Panels for Maximum Buckling Load Using Lamination Parameters
5. Optimum stacking sequence design of composite materials Part II: Variable stiffness design
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