Postbuckling of orthotropic composite plates loaded in compression
- 1 December 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 21 (12), 1729-1735
- https://doi.org/10.2514/3.8316
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- An Adaptive Finite Difference Solver for Nonlinear Two-Point Boundary Problems with Mild Boundary LayersSIAM Journal on Numerical Analysis, 1977
- The Large Deflection and Post-Buckling Behaviour of Some Laminated PlatesAeronautical Quarterly, 1973