Abstract
Mainly, this paper deals with cylindrical laminated panels, axially compressed under the constraint of four simply-supported edges.
By imposing uniform increasing end-shortening to the two opposite circular edges, characteristic equilibrium paths have been obtained in correspondence to numerical evaluations with finite element models subject to geometric non linearity. A peculiar link among different branches of the total path, each of which is connected to a proper deformed configuration, is pointed out in the axial load/end-shortening space.
Convergence problems and mesh sensibility are also examined.
Similar content being viewed by others
References
Esposito, R., Guglielmino, G., Soprano, A. and Tricomi, D., Sulla Risposta a Carichi Assiali di Tubi Conici in Vetroresina,XXI AIAS, Genova, 1992.
Calì, C. and Esposito, R., Critical Stability of Laminated Cylindrical Panels Under Axial Loads,Science and Engineering of Composite Materials,2, No. 4, 1993.
Bathe, K.J.,Finite Element Procedures in Engineering Analysis, Prentice-Hall Inc., Englewood Cliffs, 1982.
Zienkiewicz, O.C. and Taylor R.L.,The Finite Element Method, McGraw-Hill Book Company, Vol. 1/2, London, 1991.
Ochoa, O.O. and Reddy Y.N.,Finite Element Analysis of Composite Laminates, Kluwer Academic Publishers, Dordrecht, 1992.
Crisfield, M.A., A Fast Incremental/Iterative Solution Procedure that Handles “Snap-Through”,Computers and Structures 13, 1981.
Riks, E., An Incremental Approach to the Solution of Snapping and Buckling Problems,International Journal of Solids and Structures 15, 1979.
Bauld, N.R. and Khot, N.S., A Numerical and Experimental Investigation of Buckling Behaviour of Composite Panels,Computers and Structures 15, 1982.
Khot, N.S. and Bauld, N.R., Further Comparison of the Numerical and Experimental Buckling Behaviour of Composite Panels,Computers and Structures 17, 1983.
Zhang, Y. and Matthews, F.L., Large Deflection Behaviour of Simply Supported Laminated Panels Under In-Plane Loading,Journal of Applied Mechanics 52, 1985.
Argyris, J.H. and Dunne, P.C., Post Buckling Finite Element Analysis of Circular Cylinders and End Load,Forschung im Ingenieurwesen 44, 1978.
Geier, B. and Rower, K., On the Analysis Behaviour of Laminated Composite Plates and Shells,International Journal of Numerical Methods in Engineering 27, 1989.
Kohnke, P.C.,ANSYS Engineering Analysis System Theoretical Manual, Swanson Analysis System, Houston (PA), 1987.
De Salvo, G.J. and Gorman, R.W.,ANSYS Engineering System User's Manual, Swanson Analysis System, Houston (PA), 1989.
Jun, S.M. and Hong, C.S., Buckling Behaviour of Laminated Composite Cylindrical Panels Under Axial Compression,Computers and Structures 29, 1988.
Tsai, S.W.,Composite Design, Think Composites, Dayton, 1985.
Snell, M.B. and Morley, N.T., The Compression Buckling Behaviour of Highly Curved Panels of Fiber Reinforced Plastic, Proceedings of the5th International Conference on Composite Materials, The Metallurgical Society, 1985, pp. 1327–1354.
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Calì, C., Esposito, R., Graziano, M. et al. Geometrically nonlinear analysis for some axially compressed laminated cylindrical panels. Appl Compos Mater 1, 301–316 (1994). https://doi.org/10.1007/BF00568286
Received:
Accepted:
Issue Date:
DOI: https://doi.org/10.1007/BF00568286