Theoretical pressure distributions and lift, drag, and pitching moment characteristics at three values of Reynolds number presented for group of airfoil sections modified for high speed applications; effectiveness of flaps and effect of standard leading edge roughness also investigated at one value of Reynolds number.


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    Title :

    Aerodynamic characteristics of number of modified NACA four-digit-series airfoil sections


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    37 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :