Numerical analysis is carried out in this paper for thick circular cylindrical shells using higher order shell theory. In orthogonal curvilinear coordinate system, all equations are derived with the inclusion of the additional quadratic and cubic terms in the Taylor's series expansions of the both in-plane as well as the transverse displacement components for the improvement of bending behaviour of the shell. Assuming (h/R)(2)<<1, a rigorous formulation involving the reduction of a three-dimensional elasticity problem to a two-dimensional one, based partly upon the Reissner's variational principle, is presented. These equations are algebraically manipulated to be in the form of a coupled system of first-order differential equations in terms of the intrinsic dependent variables. These are then solved by a segmentation method - numerical integration technique for various combinations of material and geometric parameters. The theory is shown to result in a partial differential equation system of sixteenth order.
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INDIAN INST TECHNOL, DEPT APPL MECH, MACHINE DYNAM LAB, MADRAS 600036, TAMIL NADU, INDIAINDIAN INST TECHNOL, DEPT APPL MECH, MACHINE DYNAM LAB, MADRAS 600036, TAMIL NADU, INDIA
STANLEY, AJ
GANESAN, N
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INDIAN INST TECHNOL, DEPT APPL MECH, MACHINE DYNAM LAB, MADRAS 600036, TAMIL NADU, INDIAINDIAN INST TECHNOL, DEPT APPL MECH, MACHINE DYNAM LAB, MADRAS 600036, TAMIL NADU, INDIA
机构:
Dalian Univ Technol, State Key Lab Struct Anal Ind Equipment, Dalian 116023, Peoples R China
Shenyang Inst Aeronaut Engn, Dept Aeronaut & Astronaut, Shenyang 110034, Peoples R ChinaDalian Univ Technol, State Key Lab Struct Anal Ind Equipment, Dalian 116023, Peoples R China
Zhen, Wu
Chen Wanji
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Dalian Univ Technol, State Key Lab Struct Anal Ind Equipment, Dalian 116023, Peoples R China
Shenyang Inst Aeronaut Engn, Dept Aeronaut & Astronaut, Shenyang 110034, Peoples R ChinaDalian Univ Technol, State Key Lab Struct Anal Ind Equipment, Dalian 116023, Peoples R China