Hostname: page-component-cd9895bd7-gvvz8 Total loading time: 0 Render date: 2024-12-22T15:53:22.984Z Has data issue: false hasContentIssue false
  • English
  • Français

On the Deformation of Parallelogrammic Sandwich Panels

Published online by Cambridge University Press:  04 July 2016

J. B. Kennedy
J. B. Kennedy*
Affiliation:
Department of Civil Engineering, University of Windsor, Canada
Get access Rights & Permissions [Opens in a new window]

Extract

Sandwich panels are utilised quite often in aircraft and missile structures mainly because of their high strength to weight ratio. The core of the panel, made of light material such as balsa wood or synthetic material, stabilises the face skin sheet which is usually metallic, and contributes to the shear strength of the section.

Rectangular sandwich panels have been analysed by various investigators. In particular, Reissner deduced the range of linearity of deflections as a function of the core rigidity relative to that of the face skin. Results for parallelogrammic sandwich panels, however, are not available.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 74 , Issue 714 , June 1970 , pp. 496 - 501
Copyright
Copyright © Royal Aeronautical Society 1970 

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. Reissner, E. Finite Deflections of Sandwich Plates. Journal Aero Sci, Vol 15, 1948.Google Scholar
2. Taylor, J. L. Strength of Sandwich Panels. Proc VII Int Congress Applied Mechanics, 1948.Google Scholar
3. Libove, C. and Batdorf, S. B. A General Small Deflection Theory for Flat Sandwich Plates. NASA TR No 899, 1949.Google Scholar
4. Hoff, N. J. Bendine anH Buckling of Rectangular Sandwich Plates. NACA TN 2225, 1950.Google Scholar
5. Eringen, A. C. Bending and Buckling of Rectangular Sandwich Plates. Proc 1st US Natl Congr Appl Mech, 1951.Google Scholar
6. Ikeda, K. Theory of Bending of Isotropic Flat Sandwich Plates and its Applications. Proc 5th Japan Natl Congr for Appl Mech, 1955.Google Scholar
7. Thurston, G. A. Bending and Buckling of Clamped Sandwich Plates. Journal Aero Sci, Vol 24, 1957.Google Scholar
8. Cheng, S. On the Theory of Bending of Sandwich Plates. Proc 4th US Natl Congr Appl Mech, 1962.Google Scholar