Pandya, B. N. ; Kant, T. (1988) Finite element analysis of laminated composite plates using a higher-order displacement model Composites Science and Technology, 32 (2). pp. 137-155. ISSN 0266-3538
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Official URL: http://linkinghub.elsevier.com/retrieve/pii/026635...
Related URL: http://dx.doi.org/10.1016/0266-3538(88)90003-6
A C° continuous displacement finite element formulation of a higher-order theory for flexure of thick arbitrary laminated composite plates under transverse loads is presented. The displacement model accounts for non-linear and constant variation of in-plane and transverse displacement model eliminates the use of shear correction coefficients. The discrete element chosen is a nine-noded quadrilateral with nine degrees-of-freedom per node. Results for plate deformations, internal stress-resultants and stresses for selected examples are shown to compare well with the closed-form, the theory of elasticity and the finite element solutions with another higher-order displacement model by the same authors. A computer program has been developed which incorporates the realistic prediction of interlaminar stresses from equilibrium equations.
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|Deposited On:||13 Nov 2010 12:22|
|Last Modified:||17 May 2016 00:43|
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