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Volume 26, Issue 3
1 March 1954
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 26, Issue 3
Review Article| March 01 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 Available to Purchase

P.R. Payne
P.R. Payne
Chief Project Engineer, Auslcr Aircraft Ltd.
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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 (3): 80–84.
https://doi.org/10.1108/eb032401

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

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© MCB UP Limited
1954
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