Sandwich Construction

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 August 1960

Abstract

IN Part I of this paper, the basic equations were established for the various modes of instability of flat sandwich panels subjected to lengthwise compression. Whilst these equations are valuable in determining the strength of a given panel they do not give a direct indication of the cross‐sectional dimensions of a panel required to carry a given load, especially if the panel is to be the optimum, i.e. of minimum weight.

Citation

Heath, W. (1960), "Sandwich Construction", Aircraft Engineering and Aerospace Technology, Vol. 32 No. 8, pp. 230-235. https://doi.org/10.1108/eb033287

Download as .RIS

Publisher

:

MCB UP Ltd

Copyright © 1960, MCB UP Limited

Please note you might not have access to this content

You may be able to access this content by login via Shibboleth, Open Athens or with your Emerald account.
If you would like to contact us about accessing this content, click the button and fill out the form.
To rent this content from Deepdyve, please click the button.