Optimal laminate configurations of cylindrical shells for axial buckling

Publisher Website

1 July 1985

journal article
Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal

Vol. 23 (7), 1093-1098
https://doi.org/10.2514/3.9042

Abstract

No abstract available

This publication has 4 references indexed in Scilit:

Optimal laminated composite shells for buckling and vibration
AIAA Journal, 1983
Buckling of Angle-Ply Laminated Circular Cylindrical Shells
Journal of Applied Mechanics, 1979
Errata: "Effect of Heterogeneity on the Stability of Composite Cylindrical Shells under Axial Compression''
AIAA Journal, 1966
Effect of heterogeneity on the stability of composite cylindrical shells under axial compression.
AIAA Journal, 1966

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