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Research Reports and Memoranda

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 September 1940

Abstract

Methods are described for calculating the period and frequency of vibration of cantilever wings and similar structures in which the weight and moment of inertia vary along the span. Both the beam and torsional frequencies may be calculated by these methods. The procedure is illustrated by examples.

Citation

(1940), "Research Reports and Memoranda", Aircraft Engineering and Aerospace Technology, Vol. 12 No. 9, pp. 278-278. https://doi.org/10.1108/eb030688

Publisher

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MCB UP Ltd

Copyright © 1940, MCB UP Limited