Investigation made in 7 by 10-ft wind tunnel and in variable density wind tunnel of airfoil with various slotted flap arrangements, in order to determine airfoil section aerodynamic characteristics as affected by flap shape, slot shape, and flap location. (10¢)


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    Title :

    Wind-tunnel investigation of N.A.C.A. 23012 airfoil with various arrangements of slotted flaps


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1939


    Size :

    31 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :