Natural Vibrations of a Free Structure: Application of the Matrix Flexibility Method to the Prediction of Normal Vibration Modes Using a Co‐ordinate System Which Facilitates Programming on a Digital Computer
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 March 1962
Abstract
THE matrix flexibility method for the prediction of the normal modes of vibration of a structure may be extended to the case of a structure which has no external supports. This is of particular relevance to problems of aircraft and missile vibration.
Citation
Jennings, A. (1962), "Natural Vibrations of a Free Structure: Application of the Matrix Flexibility Method to the Prediction of Normal Vibration Modes Using a Co‐ordinate System Which Facilitates Programming on a Digital Computer", Aircraft Engineering and Aerospace Technology, Vol. 34 No. 3, pp. 81-83. https://doi.org/10.1108/eb033530
Publisher
:MCB UP Ltd
Copyright © 1962, MCB UP Limited