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.


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    Title :

    Lift on wing in propeller slipstream as related to low-speed flight


    Additional title:

    Aeronautical Eng Rev


    Contributors:

    Published in:

    Publication date :

    1956


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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