Composite cylindrical panels—optimum lay-up for buckling by ranking
- 31 December 1991
- journal article
- Published by Elsevier in Computers & Structures
- Vol. 38 (2) , 217-225
- https://doi.org/10.1016/0045-7949(91)90098-7
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Buckling behavior of laminated composite cylindrical panels under axial compressionComputers & Structures, 1988
- A doubly curved quadrilateral finite element for the analysis of laminated anisotropic thin shells of revolutionComputers & Structures, 1980
- General Panel Sizing Computer Code and Its Application to Composite Structural PanelsAIAA Journal, 1979