For purpose of providing standard airfoil characteristics for use in airplane design, Material Division of Army Air Corps requested that six airfoils having commonly used sections be tested in variable-density wind tunnel; results of tests.


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    Title :

    Tests of three tapered airfoils based on N.A.C.A. 2200 N.A.C.A.-M6, and Clark Y sections


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1934


    Size :

    8 pages


    Remarks:

    5 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :