Aerodynamic force tests conducted in vertical wind tunnel; increase of 41.5 per cent in max. lift; angle of attack for max. lift increased 13 deg.; max. increase of 30 deg. possible in highest stalling angle.


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    Title :

    Aerodynamic characteristics of slotted clark Y wing as affected by auxiliary airfoil position


    Additional title:

    Nat. Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1931


    Size :

    16 pages


    Remarks:

    31 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




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