Hostname: page-component-77c89778f8-9q27g Total loading time: 0 Render date: 2024-07-17T21:09:20.641Z Has data issue: false hasContentIssue false
  • English
  • Français

Buckling of Sandwich Panels with Laminated Face Plates

Published online by Cambridge University Press:  07 June 2016

T R A Pearce  and
J P H Webber
T R A Pearce
Affiliation:
Department of Aeronautical Engineering, University of Bristol
J P H Webber
Affiliation:
Department of Aeronautical Engineering, University of Bristol
Get access

Summary

The buckling of simply-supported sandwich panels, made up from fibre reinforced laminated face plates and honeycomb cores, is considered when they are subjected to uniform end loading. Numerical results are given for both overall buckling and face plate wrinkling for panels having typical carbon fibre faces with the laminations arranged to give effectively orthotropic properties.

Type
Research Article
Information
Aeronautical Quarterly , Volume 23 , Issue 2 , May 1972 , pp. 148 - 160
Copyright
Copyright © Royal Aeronautical Society. 1972

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. Hemp, W S On a theory of sandwich construction. ARC R & M 2672, 1952.Google Scholar
2. Tsai, S W Structural behaviour of composite materials. NASA CR-71, 1964.Google Scholar
3. Rothwell, A Optimum fibre orientations for the buckling of thin plates of composite material. Fibre Science and Technology, Vol 2, p 111, 1969.Google Scholar
4. Whitney, J M Leissa, A W Analysis of a simply supported laminated anisotropic rectangular plate. AIAA Journal, Vol 8, pp 28-33, 1970.CrossRefGoogle Scholar
5. Kuenzi, E W Buckling coefficients for simply supported, flat, rectangular sandwich panels under biaxial compression. US Forest Products Laboratory, FPL 135, 1970.Google Scholar
6. Allen, H G Analysis and Design of Structural Sandwich Panels. Pergamon Press, 1969.Google Scholar
7. Tsai, S W Azzi, V D Strength of laminated composite materials. AIAA Journal, Vol 4, pp 296-301, 1966.Google Scholar
8. Lekhnitskii, S G Anisotropic Plates. Gordon and Breach, 1968.Google Scholar
9. Lekhnitskii, S G Theory of Elasticity of an Anisotropic Elastic Body. Holden-Day, 1963.Google Scholar