Optimal laminate configurations of cylindrical shells for axial buckling
Author:
Affiliation:
1. Institute of Space and Astronautical Science, Tokyo, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9042
Reference8 articles.
1. Effect of heterogeneity on the stability of composite cylindrical shells under axial compression.
2. Buckling of Angle-Ply Laminated Circular Cylindrical Shells
3. Optimal laminated composite shells for buckling and vibration
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