To provide information that might lead to development of better propeller sections, airfoils were tested in NACA high-speed wind tunnel for study of effect of thickness form on aerodynamic characteristics; results indicate that further improvement in airfoil shapes for high-speed applications may be expected. (See also - 10c)


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    Title :

    Tests of 16 related airfoils at high speeds


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1934


    Size :

    23 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Tests of 16 related airfoils at high speeds

    Stack, John / VonDoenhoff, Albert E. | TIBKAT | 1934


    Airfoils at low speeds

    Selig, Michael S. / Donovan, John F. / Fraser, David B. | TIBKAT | 1989


    Aerodynamic Characteristics of Airfoils at High Speeds

    Briggs, L J / Hull, G F / Dryden, H L | NTRS | 1925


    Aerodynamic characteristics of airfoils at high speeds

    Briggs, L.J. / Hull, G.F. / Dryden, H.L. | Engineering Index Backfile | 1925


    Aerodynamic characteristics of airfoils at high speeds

    Briggs, L. J. / Hull, G. F. / Dryden, H. L. | TIBKAT | 1928