Analytical solution in parametric form of lift on fixed wing extending through propeller slipstream, which is valid for all slipstream-velocity/forward-flight-velocity ratios, is obtained, permitting employment of optimization techniques which should appreciably advance attack on problems of low speed flight.
Lift on wing in propeller slipstream as related to low-speed flight
Aeronautical Eng Rev
Aeronautical Engineering Review ; 15 , n 10
1956
7 pages
Aufsatz (Zeitschrift)
Englisch
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