Solution presented for relation between blade angle, thrust, and torque coefficients of rotor in hovering flight; method can be used for calculation of static thrust and torque of modern variable pitch propellers.
Static thrust analysis for helicopter rotors and airplane propellers
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 15 , n 5
1948
7 pages
Bibliography
Aufsatz (Zeitschrift)
Englisch
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