Study to determine spanwise distribution of lift increase due to slipstream at different angles of attack of wing and at different free stream to slipstream velocity ratios; empirical evaluation of destalling effects made for STOL configuration of experiment.


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    Title :

    Experimental investigation of aerodynamics of wing in slipstream


    Additional title:

    J Aeronautical Sciences


    Contributors:

    Published in:

    Publication date :

    1958


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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