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Deformation of Sandwich Structure

Published online by Cambridge University Press:  04 July 2016

H. L. Cox  and
D. W. Martin
H. L. Cox
Affiliation:
National Physical Laboratory
D. W. Martin
Affiliation:
National Physical Laboratory
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Extract

The purpose of this note is to present formulae, derived by stationary energy considerations, for the deflection of an arbitrary length of sandwich structure subjected to the three-point bend test, for comparison with experimental results.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 69 , Issue 651 , March 1965 , pp. 193 - 197
Copyright
Copyright © Royal Aeronautical Society 1965

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