The results of tests of six airfoils having the N.A.C.A. 230 mean line and varying in thickness from 0.06c to 0.21c are presented. These results agree with previous findings in showing that aerodynamically the best section is one of moderate thickness. The data are of value mainly in connection with the design of tapered wings having sections based on the N.A.C.A. 230 mean line.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

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


    Beteiligte:

    Erscheinungsdatum :

    01.05.1936


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



    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 variable-density wind tunnel

    Jacobs, E.N. / Pinkerton, R.M. | Engineering Index Backfile | 1936



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

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


    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