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The Performance of Rotating‐Wing Aircraft Rotors

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 May 1947

Abstract

THIS paper presents a summary of the method and results of a general investigation into the performance characteristics of ‘single’ autogyro and helicopter rotors, which was a preliminary to the establishment, by the firm the author serves, of a helicopter division.

Citation

Toms, C.F. (1947), "The Performance of Rotating‐Wing Aircraft Rotors", Aircraft Engineering and Aerospace Technology, Vol. 19 No. 5, pp. 150-162. https://doi.org/10.1108/eb031506

Publisher

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MCB UP Ltd

Copyright © 1947, MCB UP Limited