📖 The Scoop
Charts showing the rotor profile drag-lift ratio are presented for a helicopter rotor operating in forward flight and having hinged rectangular untwisted blades. Charts are given for a range of power input covering glides, level flight, and moderate rates of climb. Each chart expresses the relation between the lift and the profile-drag characteristics of the rotor for various combinations of pitch angle, tip-speed ratio, and solidity for a particular value of a parameter representing the shaft power output.
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