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Stability and Control of Single Rotor Helicopter with Hinged Blades: A Statement of the Elements of a Complex Subject in which the Author has Presented the Case with the Minimum Use of Mathematics

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 February 1949

Abstract

THE present paper gives, in abbreviated form, the theory of blade motion and of static and dynamic stability of single‐rotor helicopters. Limitations of space do not permit of full discussion and the article should be taken as only an introduction to the somewhat complex problems of helicopter stability and control.

Citation

Zbrozek, J.K. (1949), "Stability and Control of Single Rotor Helicopter with Hinged Blades: A Statement of the Elements of a Complex Subject in which the Author has Presented the Case with the Minimum Use of Mathematics", Aircraft Engineering and Aerospace Technology, Vol. 21 No. 2, pp. 32-38. https://doi.org/10.1108/eb031724

Publisher

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MCB UP Ltd

Copyright © 1949, MCB UP Limited