Conditions for laminated plates to remain flat under inplane loading
- 31 December 1986
- journal article
- Published by Elsevier in Composite Structures
- Vol. 6 (4) , 261-270
- https://doi.org/10.1016/0263-8223(86)90022-x
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Post-Buckling Behaviour of Simply-Supported Cross-Ply Rectangular PlatesAeronautical Quarterly, 1976
- The buckling and post-buckling behaviour of composite plates under biaxial loadingInternational Journal of Mechanical Sciences, 1975