Hostname: page-component-586b7cd67f-g8jcs Total loading time: 0 Render date: 2024-11-24T22:37:16.248Z Has data issue: false hasContentIssue false
  • English
  • Français

Torsional Vibrations of a Multi-Rotor System Having a Non-Linear Flexible Coupling

Published online by Cambridge University Press:  28 July 2016

S. Mahalingam
S. Mahalingam*
Affiliation:
Department of Mechanical Engineering, University of Ceylon
Get access Rights & Permissions [Opens in a new window]

Extract

The free and forced vibrations of a multi-rotor system where one section of the shaft has a nonlinear elastic characteristic are considered in this paper. For any frequency of steady vibration the system is reduced to an equivalent rotor at either end of the nonlinear section. The vibrations at all points are assumed to be one-term approximate solutions and the amplitudes of steady forced vibration are determined by a method outlined by the author in an earlier paper.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 61 , Issue 563 , November 1957 , pp. 779 - 781
Copyright
Copyright © Royal Aeronautical Society 1957

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. Mahalingham, S. (1957). Forced Vibration of Systems with Non-Linear, Non-Symmetrical Characteristics. Journal of Applied Mechanics, September 1957.Google Scholar
2. Brock, J. E. (1951). Iterative Numerical Method for Non-Linear Vibrations. Journal of Applied Mechanics, Vol. 18, March 1951.Google Scholar