Use of the finite strip method in predicting the behaviour of composite laminated structures
- 1 July 2002
- journal article
- Published by Elsevier in Composite Structures
- Vol. 57 (1-4) , 11-36
- https://doi.org/10.1016/s0263-8223(02)00059-4
Abstract
No abstract availableKeywords
This publication has 84 references indexed in Scilit:
- Analysis Features of VICONOPT, An Exact Buckling and Vibration Program for Prismatic Assemblies of Anisotropic PlatesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Buckling and vibration of any prismatic assembly of shear and compression loaded anisotropic plates with an arbitrary supporting structureInternational Journal of Mechanical Sciences, 1983
- Buckling and vibration of anisotropic or isotropic plate assemblies under combined loadingsInternational Journal of Mechanical Sciences, 1974
- Elastic stability of biaxially loaded longitudinally stiffened composite structuresPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Natural vibrations of thin, flat-walled structures with different boundary conditionsJournal of Sound and Vibration, 1971
- A GENERAL ALGORITHM FOR COMPUTING NATURAL FREQUENCIES OF ELASTIC STRUCTURESThe Quarterly Journal of Mechanics and Applied Mathematics, 1971
- General sinusoidal stiffness matrices for buckling and vibration analyses of thin flat-walled structuresInternational Journal of Mechanical Sciences, 1968
- Bending, Buckling and Vibration of Orthotropic Plate-Beam StructuresJournal of Ship Research, 1968
- A Unified Approach to the Initial Buckling of Stiffened Panels in CompressionAeronautical Quarterly, 1968
- THE FINITE STRIP METHOD IN THE ANALYS OF ELASTIC PLATES WITH TWO OPPOSITE SIMPLY SUPPORTED ENDS.Proceedings of the Institution of Civil Engineers, 1968