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Optimization of Variable-Stiffness Panels for Maximum Buckling Load Using Lamination Parameters

✍ Scribed by Ijsselmuiden, Samuel T.; Abdalla, Mostafa M.; Gürdal, Zafer


Book ID
127305867
Publisher
American Institute of Aeronautics and Astronautics
Year
2010
Tongue
English
Weight
436 KB
Volume
48
Category
Article
ISSN
0001-1452

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Optimal design of symmetric laminates wi
✍ M. Walker 📂 Article 📅 1999 🏛 Elsevier Science 🌐 English ⚖ 305 KB

Finite element solutions are presented for the optimal design of symmetrically laminated rectangular plates with central circular cut-outs subject to a combination of simply supported, clamped and free boundary conditions. The design objective is the maximisation of the biaxial buckling load by dete