Large deflection behavior of circular quasi-isotropic laminates under point loading
- 1 January 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 25 (1), 99-106
- https://doi.org/10.2514/3.9587
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Large deflections of circular isotropic membranes subjected to arbitrary axisymmetric loadingComputers & Structures, 1985
- Prediction of low-velocity impact damage in thin circular laminatesAIAA Journal, 1985