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
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
:MCB UP Ltd
Copyright © 1954, MCB UP Limited