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The Problem of Rotating n‐Bladed Laminae

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 March 1946

Abstract

CONSIDER an n‐bladed lamina in the z plane, rotating with angular velocity w, the length of each blade being a. Consider the transformation

Citation

Jacobs, I.J.A. (1946), "The Problem of Rotating n‐Bladed Laminae", Aircraft Engineering and Aerospace Technology, Vol. 18 No. 3, pp. 89-96. https://doi.org/10.1108/eb031346

Publisher

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MCB UP Ltd

Copyright © 1946, MCB UP Limited