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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

A. Jennings (Lecturer in Aircraft Structures, Civil Engineering Department, University of Manchester, Manchester 13)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 March 1962

55

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

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MCB UP Ltd

Copyright © 1962, MCB UP Limited

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