This paper extends the work of Parts I and II to forward flight conditions, and completes the work on gust clearances.
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 ; 26 , 3 ; 80-84
01.03.1954
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Rotor Blade Motion in a Vertical Sharp-edged Gust
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