In Part 1 it is shown that the equation for blade equilibrium about the flapping pin is
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 ; 26 , 2 ; 41-45
1954-02-01
5 pages
Article (Journal)
Electronic Resource
English
Rotor blade motion in vertical sharp-edged gust
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