journal article·1989-01

A practical approach to optimal design of laminated cylindrical shells for buckling

G. Sun

Composites Science and Technology· Volume 36· Issue 3
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Abstract

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Research context

OpenAlex topics: Composite Structure Analysis and Optimization · Topology Optimization in Engineering · Structural Analysis and Optimization

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References (10)

Show source-provided references
1. Optimum design of laminated plates under axial compression10.2514/3.61269 ↗
2. Optimum design of laminated plates under shear10.1177/002199837901300406 ↗
3. Design of laminated plates for maximum stiffness10.1177/002199838401800105 ↗
4. Optimal fibre orientation for simply-supported, angle-ply plates under biaxial compression10.1016/0263-8223(88)90005-0 ↗
5. Optimization of laminated composite plates and shells
6. Optimal laminated composite shells for buckling and vibration10.2514/3.8090 ↗
7. Optimal laminate configurations of cylindrical shells for axial buckling10.2514/3.9042 ↗
8. Optimal design of laminated-composite circular-cylindrical shells subjected to combined loads10.1115/1.3173619 ↗
9. Jiang · Acta Materiae Compositae Sinica · 1985 · 2 · 13
10. Kuester · 1973