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Rotor Blade Motion in a Vertical Sharp‐Edged Gust: A Stud/ of the Dynamics of Helicopter Blade Flapping with a Method of Deriving Maximum Gust Deflexion

P.R. Payne (Chief Project Engineer, Auslcr Aircraft Ltd.)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 March 1954

Abstract

This paper extends the work of Parts I and II to forward flight conditions, and completes the work on gust clearances.

Citation

Payne, P.R. (1954), "Rotor Blade Motion in a Vertical Sharp‐Edged Gust: A Stud/ of the Dynamics of Helicopter Blade Flapping with a Method of Deriving Maximum Gust Deflexion", Aircraft Engineering and Aerospace Technology, Vol. 26 No. 3, pp. 80-84. https://doi.org/10.1108/eb032401

Publisher

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MCB UP Ltd

Copyright © 1954, MCB UP Limited