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Structural analog for sandwich panels with finite deflections

Published online by Cambridge University Press:  04 July 2016

H. H. Al-Qarra
H. H. Al-Qarra*
Affiliation:
SDC, PO Box 87132, Riyadh 11642, Saudi Arabia
*
*Formerly, Department of Civil Engineering, University of Southampton.
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Abstract

The solution of sandwich plate problems by the framework method is proposed and the basic elements of the method used are reviewed. The technique is demonstrated by application to a simple framework analog for rectangular sandwich panels with very thin faces and an antiplane core. A number of illustrative examples involving small and large deflections are solved.

Type
Research Article
Information
The Aeronautical Journal , Volume 94 , Issue 933 , March 1990 , pp. 99 - 106
Copyright
Copyright © Royal Aeronautical Society 1990 

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