Aerodynamic force tests made in wind tunnel using highly tapered Clark Y wing equipped with various split flaps; results given for both full and partial span split flaps.


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    Title :

    Effects of full-span and partial-span split flaps on aerodynamic characteristics of tapered wing


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:


    Publication date :

    1934


    Size :

    6 pages


    Remarks:

    5 Supp plates, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English