Hostname: page-component-cd9895bd7-fscjk Total loading time: 0 Render date: 2024-12-28T06:00:28.682Z Has data issue: false hasContentIssue false
  • English
  • Français

Natural Frequencies of Constant Thickness Cantilever Triangular Plates oj Arbitrary Plan Form

Published online by Cambridge University Press:  28 July 2016

Bertram Klein
Bertram Klein*
Affiliation:
Los Angeles, California
Get access Rights & Permissions [Opens in a new window]

Extract

Simple Formulae are presented for the first three bending-type and the first torsion-type natural frequencies of any constant thickness cantilever triangular plate. The formulae are derived by a semi-empirical method. Comparison of calculated frequencies with test values indicates agreement within a few per cent. for a variety of plate plan forms.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 60 , Issue 544 , April 1956 , pp. 281 - 282
Copyright
Copyright © Royal Aeronautical Society 1956

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. Gustafson, P. N., Stokey, W. F., and Zorowski, C. F. (1953). An Experimental Study of Natural Vibrations of Cantilevered Triangular Plates. Journal of the Aeronautical Sciences, Vol. 20, No. 5, pp. 331–337, May 1953.Google Scholar
2. Anderson, B. W. (1954). Vibration of Triangular Cantilever Plates by the Ritz Method. Journal of Applied Mechanics, Vol. 21, pp. 365–370, 1954.Google Scholar