Hostname: page-component-78c5997874-lj6df Total loading time: 0 Render date: 2024-11-05T10:20:13.980Z Has data issue: false hasContentIssue false

The Buckling and Bending of Orthotopic Sandwich Panels With All Edges Simply-Supported

Published online by Cambridge University Press:  07 June 2016

J. R. Robinson*
Affiliation:
Handley Page Limited
Get access

Summary

A formula is derived for the buckling in compression of an orthotropic sandwich panel, with all edges simply-supported. Two special types of symmetrical sandwiches, that of a sandwich having zero core flexural stiffnesses and of a corrugated core sandwich, are considered, and curves giving the critical buckling end load per inch are presented. An approximate theory is also given for the bending of sandwich panels under the action of an axial compressive load and a uniform lateral pressure. Curves are presented giving the maximum bending moments in a corrugated core sandwich panel.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society. 1955

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.)

References

1. Libove, C. and Batdorf, S. B. A General Small-Deflection Theory for Flat Sandwich Plates. N.A.C.A. Report 899 (formerly N.A.C.A. T.N. 1526), 1948.Google Scholar
2. Timoshenko, S. Theory of Elastic Stability. McGraw-Hill, 1936.Google Scholar
3. Libove, and Hubka, . Elastic Constants for Corrugated Core Sandwich Plates. N.A.C.A. T.N. 2289, 1950.Google Scholar
4. Hemp, W. S. On a Theory of Sandwich Construction. R. & M. 2672, 1952.Google Scholar
5. Tyson, F. Metal Sandwich Construction. Royal Aeronautical Society Section Lecture on 2nd March 1954.Google Scholar