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Volume 12, Issue 9
1 September 1940
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 12, Issue 9
Review Article| September 01 1940

Research Reports and Memoranda

Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1940
Aircraft Engineering (1940) 12 (9): 278.
https://doi.org/10.1108/eb030688

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.

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© MCB UP Limited
1940
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