Postbuckling behavior of laminated plates using a direct energy-minimization technique
Authors:
- 1 December 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 27 (12) , 1785-1792
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- Simple expressions for higher vibration modes of uniform Euler beamsAIAA Journal, 1988
- Buckling and failure of sandwich plates with graphite-epoxy faces and various coresJournal of Aircraft, 1988
- Buckling analysis of anisotropic sandwich plates faced with fiber-reinforced plasticsAIAA Journal, 1985
- Buckling, postbuckling, and crippling of materially nonlinear laminated composite platesInternational Journal of Solids and Structures, 1984
- A refined nonlinear theory of plates with transverse shear deformationInternational Journal of Solids and Structures, 1984
- Stress Analysis of Thick Laminated Composite and Sandwich Plates*Journal of Composite Materials, 1972
- General instability and face wrinkling of sandwich plates - Unified theory and applications.AIAA Journal, 1967
- Influence of Rotatory Inertia and Shear on Flexural Motions of Isotropic, Elastic PlatesJournal of Applied Mechanics, 1951
- The Effect of Transverse Shear Deformation on the Bending of Elastic PlatesJournal of Applied Mechanics, 1945