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Volume 26, Issue 2
1 February 1954
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 26, Issue 2
Review Article| February 01 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

P.R. Payne
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Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1954
Aircraft Engineering (1954) 26 (2): 41–45.
https://doi.org/10.1108/eb032391

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

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1954
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