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Governing Equations for Thick Sandwich Shells with Honeycomb Cores and Laminated Faces

Published online by Cambridge University Press:  07 June 2016

J P H Webber
J P H Webber*
Affiliation:
Department of Aeronautical Engineering, University of Bristol
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Summary

The governing elasticity equations for sandwich shells of double curvature are discussed. No restriction is placed on the thickness of the honeycomb core, and the faces are taken to be made up from fibre reinforced plastic laminations. Some numerical results are given for a circular cylinder subjected to uniform internal radial loading. The results show the importance of treating the core as a thick shell, and of including the bending effects and coupling terms in the laminated faces.

Type
Research Article
Information
Aeronautical Quarterly , Volume 25 , Issue 4 , November 1974 , pp. 271 - 286
Copyright
Copyright © Royal Aeronautical Society. 1974

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References

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