Postbuckling behavior of selected curved stiffened graphite-epoxy panels loaded in axial compression
- 15 April 1985
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Postbuckling Behaviour of Cylindrically Curved Panels of Generally Layered Composite Materials with Small Initial Imperfections of GeometryPublished by Springer Nature ,1983
- Postbuckling behavior of selected flat stiffened graphite-epoxy panels loaded in compressionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- General Panel Sizing Computer Code and Its Application to Composite Structural PanelsAIAA Journal, 1979
- Buckling and post-buckling of orthotropic laminated platesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- The buckling and post-buckling behaviour of composite plates under biaxial loadingInternational Journal of Mechanical Sciences, 1975
- The Large Deflection and Post-Buckling Behaviour of Some Laminated PlatesAeronautical Quarterly, 1973
- Buckling and postbuckling behavior of composite cylindrical shells under axial compressionAIAA Journal, 1970