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Abstract
The bubHing of laminated composite cylindrical shell panels subjected to transverse load is investigated. The geometrical non-linear analysis is carried out using thefinite element method based o,n a higher-order shear deformation theory. An eight nodded degenerated isoparametric shell element with nine degrees of freedom at each node is considered. The geometric non-linear behaviour and the collapse pressures ere presented for symmetrically and antisymmetrically laminated cross-ply and angle-ply cylindrical shell panels subiected to uniform normal pressure.
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References
- Bauld Jr, N.R. and Khot, N.S., "A Numerical and Experimental Investigation of the Buckling Behavior of Composite Panels", Computers and Structures, Vol. 15, pp.393-403, 1982.
- Jun, S.M. and Hong, C.S., "Buckling Behavior of Laminated Composite Cylindrical Panels under Axial Compression", Computers and Structures, Y o1.29, pp. 479-490, 1988.
- Palazotto, A.N. and Tisler, T.W., "Considerations of Cutouts in Composite Cylindrical Panels", Computers and Structures, Vol. 29, pp. 1101-1110, 1988.
- Goldmanis, M. and Riekstinsh, A., "Post-Buckling Finite Element Analysis of Composite Cylindrical Panels in Axial Compression", Composite Structures, Vol.29, pp. 457-462, 1994.
- Noor, A.K., Starnes Jr, J.H. and Peters, J.M., "Nonlinear and Post-Buckling Responses of Curved Composite Panels with Cutouts", Composite Structures, Vol. 34, pp. 213-240, 1996.
- Chaplin, C.P. and Palazotto, A.N., "The Collapse of Composite Cylindrical Panels with Various Thickness using Finite Element Analysis", Computers and Structures, Vol.60, pp. 797 -815, 1996.
- Simitses, G.J., "Buckling of Moderately Thick Laminated Cylindrical Shells : A Review", Composites Part B, Vol. 27B, pp. 581-587, 1996.
- Kim, K.D., "Buckling Behaviour of Composite panels Using the Finite Element Method", Composite Structures, Vol. 36, pp. 33-43, 1996.
- Kim, K. and Voyiadjis, G.Z., "Non-linear Finite Element Analysis of Composite panels,', Composites Part B, Vol. 30, pp.365-381, 1999.
- Prema Kumar, W.P. and Palaninathan, R., "Non-linear Response olaminated Cylindrical panels',, Thin Walled Structures, Vol.39, pp. 519-533, 2001.
- Hilburger, M.W., Britt, V.O. and Nameth, M.p., "Buckling Behavior of Compression Loaded euasiisotropic Curved Panels with a Circular Cutout", Int. J. Solids and Structures, Vol.38, pp. 1495-1522, 200t.
- Sai Ram, K.S. and Sreedhar Babu, T., "Buckling of Laminated Composite Shells under Transverse Load", Composite Structures, Vol.55, pp. 157-168, 2002.
- Cook, R.D., Malkus, D.S. and Plesha, M.E.. "Concepts and Applications of Finite Elements Analysis". Chapter 12, John Wiley, New York, 1989.
- Zienkiewicz, O.C. and Taylor, R.L., "The Finite Element Method", Chapter 5, Vol.2, McGraw-Hill, London. 1991.
- Bathe, K.J., "Finite Element procedures". prentice Hall Englewood Cliffs, New Jersey, 1996.
References
Bauld Jr, N.R. and Khot, N.S., "A Numerical and Experimental Investigation of the Buckling Behavior of Composite Panels", Computers and Structures, Vol. 15, pp.393-403, 1982.
Jun, S.M. and Hong, C.S., "Buckling Behavior of Laminated Composite Cylindrical Panels under Axial Compression", Computers and Structures, Y o1.29, pp. 479-490, 1988.
Palazotto, A.N. and Tisler, T.W., "Considerations of Cutouts in Composite Cylindrical Panels", Computers and Structures, Vol. 29, pp. 1101-1110, 1988.
Goldmanis, M. and Riekstinsh, A., "Post-Buckling Finite Element Analysis of Composite Cylindrical Panels in Axial Compression", Composite Structures, Vol.29, pp. 457-462, 1994.
Noor, A.K., Starnes Jr, J.H. and Peters, J.M., "Nonlinear and Post-Buckling Responses of Curved Composite Panels with Cutouts", Composite Structures, Vol. 34, pp. 213-240, 1996.
Chaplin, C.P. and Palazotto, A.N., "The Collapse of Composite Cylindrical Panels with Various Thickness using Finite Element Analysis", Computers and Structures, Vol.60, pp. 797 -815, 1996.
Simitses, G.J., "Buckling of Moderately Thick Laminated Cylindrical Shells : A Review", Composites Part B, Vol. 27B, pp. 581-587, 1996.
Kim, K.D., "Buckling Behaviour of Composite panels Using the Finite Element Method", Composite Structures, Vol. 36, pp. 33-43, 1996.
Kim, K. and Voyiadjis, G.Z., "Non-linear Finite Element Analysis of Composite panels,', Composites Part B, Vol. 30, pp.365-381, 1999.
Prema Kumar, W.P. and Palaninathan, R., "Non-linear Response olaminated Cylindrical panels',, Thin Walled Structures, Vol.39, pp. 519-533, 2001.
Hilburger, M.W., Britt, V.O. and Nameth, M.p., "Buckling Behavior of Compression Loaded euasiisotropic Curved Panels with a Circular Cutout", Int. J. Solids and Structures, Vol.38, pp. 1495-1522, 200t.
Sai Ram, K.S. and Sreedhar Babu, T., "Buckling of Laminated Composite Shells under Transverse Load", Composite Structures, Vol.55, pp. 157-168, 2002.
Cook, R.D., Malkus, D.S. and Plesha, M.E.. "Concepts and Applications of Finite Elements Analysis". Chapter 12, John Wiley, New York, 1989.
Zienkiewicz, O.C. and Taylor, R.L., "The Finite Element Method", Chapter 5, Vol.2, McGraw-Hill, London. 1991.
Bathe, K.J., "Finite Element procedures". prentice Hall Englewood Cliffs, New Jersey, 1996.