Optimization of Cylinders with Holes under Bending using Nonconventional Laminates
Author:
Affiliation:
1. University of South Carolina, Columbia
2. The Boeing Company
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1377
Reference23 articles.
1. Design Guidelines in Nonconventional Composite Laminate Optimization
2. Optimisation of Anisotropic Composite Plates Incorporating Non-Conventional Ply Orientations
3. Effects of Size and Location of a Circular Cutout on Buckling and Failure of a Cylindrical Shell in Bending
4. W
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