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

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 February 1954

Abstract

In Part 1 it is shown that the equation for blade equilibrium about the flapping pin is

Citation

Payne, P.R. (1954), "Rotor Blade Motion in a Vertical Sharp‐edged Gust: A Study of the Dynamics of Helicopter Blade Flapping with a Method of Deriving Maximum Gust Deflexion", Aircraft Engineering and Aerospace Technology, Vol. 26 No. 2, pp. 41-45. https://doi.org/10.1108/eb032391

Publisher

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MCB UP Ltd

Copyright © 1954, MCB UP Limited