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ESTIMATION OF INTERLAMINAR STRESSES IN FIBER REINFORCED COMPOSITE CYLINDRICAL-SHELLS

DSpace at IIT Bombay

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Title ESTIMATION OF INTERLAMINAR STRESSES IN FIBER REINFORCED COMPOSITE CYLINDRICAL-SHELLS
 
Creator KANT, T
MENON, MP
 
Subject internal-pressure
finite-element
 
Description A C0 finite element formulation for flexure-membrane coupling behavior of symmetric and asymmetric laminated cylindrical shells based on a higher-order displacement model is presented. This theory incorporates a realistic nonlinear variation of displacements through the shell thickness, and eliminates the use of shear correction coefficient/s. This discrete element chosen is a nine-noded quadrilateral with nine degrees of freedom per node. The solutions are obtained through two formulations: (1) the geometrically thin shell formulation, based on the assumption that the ratio of thickness to radius of the shell is very much less than unity, and (2) the geometrically thick shell formulation, in which (h/R)2
 
Publisher PERGAMON-ELSEVIER SCIENCE LTD
 
Date 2011-08-24T07:39:01Z
2011-12-26T12:56:48Z
2011-12-27T05:46:03Z
2011-08-24T07:39:01Z
2011-12-26T12:56:48Z
2011-12-27T05:46:03Z
1991
 
Type Article
 
Identifier COMPUTERS & STRUCTURES, 38(2), 131-147
0045-7949
http://dx.doi.org/10.1016/0045-7949(91)90092-Z
http://dspace.library.iitb.ac.in/xmlui/handle/10054/10806
http://hdl.handle.net/10054/10806
 
Language en