Hostname: page-component-78c5997874-s2hrs Total loading time: 0 Render date: 2024-11-03T01:53:05.379Z Has data issue: false hasContentIssue false
  • English
  • Français

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
Get access Rights & Permissions [Opens in a new window]

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

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)