Outline of methods for calculating response of rotary wing airplanes to arbitrary control displacements. Before Inst Aeronautical Sciences.
Response of helicopters with articulated rotors to cyclic blade pitch control
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 11 , n 4
1944
11 pages
Bibliography
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
The Effects of Blade Flexibility on the Control Response of an Articulated-Rotor Helicopters
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