Hostname: page-component-74656f9884-54qdv Total loading time: 0 Render date: 2026-11-10T05:05:59.935Z Has data issue: false hasContentIssue false
  • English
  • Français

Clamped Skew Plate under Uniform Normal Loading

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

In their paper in the February 1967 Journal, Iyengar and Srinivasan have presented a solution to the problem of uniformly loaded clamped skew plates by employing characteristic functions for the modes of vibration of clamped-clamped beams. They compared their theoretical results with those obtained by Morley and Kennedy.

The writer has recently extended the 3-parameter solution by assuming a deflection function in the form:

Information

Type
Technical Notes
Information
The Aeronautical Journal , Volume 72 , Issue 688 , April 1968 , pp. 338 - 339
Copyright
Copyright © Royal Aeronautical Society 1968 

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.)

Article purchase

Temporarily unavailable

References

12. Ng, S. F. Analysis of Clamped Skewed Plates Subjected to Lateral Uniform Loading. MASc Thesis, University of Windsor, 1964.Google Scholar
13. Fung, Y. C., De Groff, H. M. and Williams, M. L. Theoretical and Experimental Effect of Sweep Upon Stress and Deflection Distribution in Aircraft Wings of High Solidity. US Air Force Technical Report No 5761, Parts 1,2,3 and 5, 1949-50.Google Scholar
14. Ng, S. F. and Kennedy, J. B. The Behaviour of Clamped Parallelogrammic Panels with Large Deflections. Sub mitted to the Fourth US South-eastern Conference on Theoretical and Applied Mechanics.Google Scholar