Research Reports and Memoranda
Aircraft Engineering and Aerospace Technology
Article publication date: 1 September 1940
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.
(1940), "Research Reports and Memoranda", Aircraft Engineering and Aerospace Technology, Vol. 12 No. 9, pp. 278-278. https://doi.org/10.1108/eb030688
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