Propellers were mounted in front of liquid cooled engine nacelle and were tested at 15 different blade angles in range from -7 1/2° to 35° at 0.75R; test rig was located outdoors and tests were made under conditions of approximately zero wind velocity; airfoil characteristics computed from statictest data, were considerably different from airfoil characteristics computed from wind tunnel test data.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Static thrust and power characteristics of six full-scale propellers


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:
    Hartman, E.P. (Autor:in) / Biermann, D. (Autor:in)


    Erscheinungsdatum :

    1940


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Static Thrust and Power Characteristics of Six Full-Scale Propellers

    Hartman, Erwin P / Biermann, David | NTRS | 1940


    Static thrust of airplane propellers

    Diehl, Walter S | NTRS | 1934


    Static thrust of airplane propellers

    Diehl, W.S. | Engineering Index Backfile | 1932


    Static thrust of airplane propellers

    Diehl, Walter S. | TIBKAT | 1932


    Tests on propellers under static thrust conditions

    Brusse, J. / Cronk, A. E. / Kettleborough, C. F. | TIBKAT | 1969