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
:MCB UP Ltd
Copyright © 1954, MCB UP Limited