Wind-tunnel studies of the performance of multirotor configurations
Description:
Report presenting the power requirements measured in static thrust and in level forward flight for two helicopter rotor configurations. One is a coaxial rotor arrangement with the rotors spaced approximately 19 percent of the rotor radius; the other is a tandem configuration in which the rotor-shaft spacing is 3 percent greater than the rotor diameter and in which the rotors lie in the same plane.
Date:
August 1954
Creator:
Dingeldein, Richard C.
Item Type:
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