Hostname: page-component-586b7cd67f-dlnhk Total loading time: 0 Render date: 2024-11-25T17:18:25.435Z Has data issue: false hasContentIssue false
  • English
  • Français

Buckling of Orthotropic Circular Plates

Published online by Cambridge University Press:  04 July 2016

K. A. V. Pandalai  and
Sharad A. Patel
K. A. V. Pandalai
Affiliation:
Department of Aeronautical Engineering, Madras Institute of Technology, India
Sharad A. Patel
Affiliation:
from Polytechnic Institute of Brooklyn, New York, Madras Institute of Technology, India
Get access Rights & Permissions [Opens in a new window]

Extract

This Note is concerned with the axisymmetric buckling of orthotropic circular plates. A circular plate fabricated with radial and/or circumferential reinforcements may be idealised as an orthotropic plate of uniform thickness h having different material properties in the radial and circumferential directions.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 69 , Issue 652 , April 1965 , pp. 279 - 280
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.)

References

1.Timoshenko, S. and Woinosky-Krieger, S.Theory of Plates and Shells. McGraw-Hill Book Co., New York, 1959; 2nd Edition, Chap. XI, p. 364.Google Scholar
2.Timoshenko, S.Theory of Elastic Stability. McGraw-Hill Book Co., New York, 1936; 1st Edition, Chap. VII, p. 368.Google Scholar