Strength and stiffness of sandwich panels under transverse loading
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 October 1971
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