Results of tests of six airfoils having N A C A 230 mean line and varying in thickness from 0.00c to 0.21c; results agree with previous findings in showing that aerodynamically best section is one of moderate thickness.


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    Title :

    Tests of N.A.C.A. Airfoils in variable-density wind tunnel


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:


    Publication date :

    1936


    Size :

    5 pages


    Remarks:

    Supp sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Tests of N.A.C.A. airfoils in variable-density wind tunnel, series 24

    Jacobs, E.N. / Ward, K.E. | Engineering Index Backfile | 1932



    Tests of N.A.C.A. airfoils in the variable-density wind tunnel Series 230.

    Jacobs, Eastman N / Pinkerton, Robert M | NTRS | 1936


    Tests of N.A.C.A. Airfoils in variable-density wind tunnel, series 4e and 63

    Jacobs, E.N. / Pinkerton, R.M. | Engineering Index Backfile | 1931


    Tests of N.A.C.A. airfoils in the variable-density wind tunnel ; 5: Series 24

    Jacobs, Eastman N. / Ward, Kenneth E. | TIBKAT | 1931