Hostname: page-component-848d4c4894-sjtt6 Total loading time: 0 Render date: 2024-06-29T08:33:00.221Z Has data issue: false hasContentIssue false
  • English
  • Français

Fundamental Frequencies of Arbitrarily Shaped Simply-Supported Triangular Plates

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

A simple set of curves is presented from which may be calculated the lowest natural frequency of flexural vibration of practically any triangular plate of constant thickness and with simply-supported edges. In many cases the results are self checking since the calculations usually may be carried out in three independent ways and compared.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 60 , Issue 541 , January 1956 , pp. 63 - 64
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. Cox, H. L. and Klein, B. (1955). Vibration of Isosceles Triangular Plates. Zeitschrift für Angewendte Mathematik and Physik (ZAMP), January 1955.Google Scholar
2. Cox, H. L. and Klein, B. (1955). Vibration of Clamped Triangular Plates. Journal of the Acoustical Society of America, May 1955.Google Scholar