Buckling and postbuckling of laminated composite plates with ply dropoffs
- 1 October 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 27 (10) , 1392-1398
- https://doi.org/10.2514/3.10276
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Influence of mechanical couplings on the buckling and postbuckling of anisotropic platesAIAA Journal, 1988
- Analytical and experimental studies on the buckling of laminated thin-walled structuresPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Buckling of unsymmetric composite laminatesComposite Structures, 1986
- Development and test verification of the Ariane 4 interstage 2/3 in CFRPPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Finite elements based on consistently assumed stresses and displacementsFinite Elements in Analysis and Design, 1985
- Response and failure analysis of a graphite-epoxy laminate containing terminating internal pliesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Approximate Solutions for Unsymmetrically Laminated PlatesJournal of Composite Materials, 1969
- Vibration of Rectangular Plates by the Ritz MethodJournal of Applied Mechanics, 1950
- On the analysis of experimental observations in problems of elastic stabilityProceedings of the Royal Society of London. Series A, Containing Papers of a Mathematical and Physical Character, 1932