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Volume 43, Issue 10
1 October 1971
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 43, Issue 10
Review Article| October 01 1971

Strength and stiffness of sandwich panels under transverse loading

MARCUS LANGLEY, C.Eng., F.R.Ae.S., F.I.Mech.E.
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Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1971
Aircraft Engineering (1971) 43 (10): 11–15.
https://doi.org/10.1108/eb034819

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.

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© MCB UP Limited
1971
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