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Strength and stiffness of sandwich panels under transverse loading

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 October 1971

57

Abstract

THIS paper describes work done to translate the theory of Structural Sandwich Panel Design into a form in which it could be used for rapid estimation in a design office.

Citation

LANGLEY, M. (1971), "Strength and stiffness of sandwich panels under transverse loading", Aircraft Engineering and Aerospace Technology, Vol. 43 No. 10, pp. 11-15. https://doi.org/10.1108/eb034819

Publisher

:

MCB UP Ltd

Copyright © 1971, MCB UP Limited

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