Postbuckling behavior of composite-stiffened-curved panels loaded in compression
- 1 June 1982
- journal article
- Published by Springer Science and Business Media LLC in Experimental Mechanics
- Vol. 22 (6), 231-236
- https://doi.org/10.1007/bf02326363
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Buckling Behavior and Structural Efficiency of Open-Section Stiffened Composite Compression PanelsAIAA Journal, 1976
- Buckling of eccentrically stringer-stiffened cylindrical panels under axial compressionComputers & Structures, 1976
- EXPLOITING SYMMETRIES FOR EFFICIENT POST-BUCKLING ANALYSIS OF COMPOSITE PLATESPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Analytical and experimental study of structurally efficient composite hat-stiffened panels loaded in axial compressionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- 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
- Buckling and vibration of anisotropic or isotropic plate assemblies under combined loadingsInternational Journal of Mechanical Sciences, 1974
- Postbuckling Behavior of Unsymmetrically Layered Anisotropic Rectangular PlatesJournal of Applied Mechanics, 1974
- The Large Deflection and Post-Buckling Behaviour of Some Laminated PlatesAeronautical Quarterly, 1973
- SYNOPTIC: Finite Deflection Discrete Element Analysis of Sandwich Plates and Cylindrical Shells with Laminated FacesAIAA Journal, 1970