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Load-deflection curves for an axially compressed cylindrical shell with normalized imperfections of various amplitudes

FROM:
Y. Venkata Narayana (1), Jagadish Babu Gunda (2), P. Ravinder Reddy (3) and R. Markandeya (4)
(1) Department of Mechanical Engineering, Sree Nidhi Institute of Science and Technology, Ghatkesar, Andrapradesh, India
(2) Advanced Systems Laboratory, Kanchan Bagh, Hyderabad, India
(3) Department of Mechanical Engineering, Chaitanya Bharathi Institute of Science and Technology, Gandipet, Andrapradesh, India
(4) Department of Metallurgical Engineering Jntu Kukatpally, Andraprdesh, India
“Nonlinear buckling and post-buckling analysis of imperfect cylindrical shells subjected to axial compressive load”, Journal of Structural Engineering, Vol. 42, No. 2, pp 78-85, June-July 2015

ABSTRACT: Imperfection sensitivity of cylindrical shells subjected to axial compressive load is investigated by means of nonlinear buckling analysis and post-buckling analysis. Nonlinear buckling analysis involves the determination of the equilibrium path (or load-deflection curve) upto the limit point load by using the Newton-Raphson approach, whereas post-buckling analysis involves the determination of the equilibrium path beyond the limit point and upto the collapse load by using the arc-length approach. Limit point loads evaluated from these two approaches for various imperfection magnitudes show an excellent agreement, which clearly confirms the numerical results obtained. Finally, the influence of L/D and R/t ratios on post-buckling behavior of isotropic and composite cylindrical shells is briefly highlighted.

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