BENDING THEORY FOR MULTILAYER ORTHOTROPIC SANDWICH PLATES

被引:24
作者
AZAR, JJ
机构
[1] University of Tulsa, Aerospace Engineerin, Tulsa, OK
关键词
D O I
10.2514/3.4950
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The governing equations on bending of multilayered orthotropic (both core and facings) sandwich plates are developed through the use of variational methods. The plate is assumed to consist of j facings and (j - 1) cores, having different thicknesses and possessing different orthotropic elastic properties. In-plane stresses in the cores are neglected as is the variation of stresses across the facings. The developed theory is an extension of that given in Ref. 7. © 1968 American Institute of Aeronautics and Astronautics, Inc., All rights reserved.
引用
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页码:2166 / +
页数:1
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