Aerodynamics force tests made in N.A.C.A. 7 by 10-ft wind tunnel on model wing with 20% chord split flap deflected 60° downward; results given in form of curves of lift, drag, and center of pressure.


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    Title :

    Effect of partial-span split flaps on aerodynamic characteristics of clark Y wing


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:


    Publication date :

    1933


    Size :

    5 pages


    Remarks:

    4 Supp Sheets


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English