Postbuckling behaviour of a blade-stiffened composite panel loaded in uniaxial compression
- 1 May 2000
- journal article
- Published by Elsevier BV in Composites Part A: Applied Science and Manufacturing
- Vol. 31 (5), 459-468
- https://doi.org/10.1016/s1359-835x(99)00085-8
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Buckling mode transition in hat-stiffened composite panels loaded in uniaxial compressionComposite Structures, 1997
- Postbuckling behaviour of hat-stiffened thin-skinned carbon-fibre composite panelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Buckling and postbuckling of composite structuresComposites, 1995
- Postbuckling Failure of Composite PanelsPublished by Springer Science and Business Media LLC ,1985