Modeling of plate flexure satisfying normal stress conditions at the plate surfaces

Vijayakumar, K. ; Krishna Murty, A. V. (1987) Modeling of plate flexure satisfying normal stress conditions at the plate surfaces Journal of the Aeronautical Society of India, 39 (4). pp. 165-172. ISSN 0001-9267

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Abstract

Modeling of plate flexure, based on cubic variation of inplane displacements and quartic variation of the normal displacement has been discussed. Displacement functions satisfy the zero shear stress condition at top and bottom surfaces of the plate. The normal stress condition at the surfaces of the plate and the elemental equilibrium eqUlltions are enforced through the use of the Lagrangian multipliers in the variational procedure used. Several new models are available as special cases in this formulation. An illustrative example of a simply-supported plate subjected to sinusoidal loading is included to indicate relative merits of the special cases.

Item Type:Article
Source:Copyright of this article belongs to Aeronautical Society of India.
ID Code:94105
Deposited On:17 Jul 2012 09:46
Last Modified:19 May 2016 07:00

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