Wind tunnel of National Advisory Committee for Aeronautics is of double-return flow type with 30 by 60-ft open jet at test section; air circulated by two propellers 35 ft 5 in. in diam, located side by side, and each directly connected to 4000-hp slip-ring induction motor; motor-control equipment permits varying speed in 24 steps between 25 and 118 mph; 6-component type balance; calibration and tests.


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    Titel :

    N.A.C.A. full-scale wind tunnel


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:


    Erscheinungsdatum :

    1933


    Format / Umfang :

    10 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    The N.A.C.A. full-scale wind tunnel

    De France, Smith J. | TIBKAT | 1933


    N.A.C.A. Variable-density wind tunnel

    Jacobs, E.N. / Abbott, I.H. | Engineering Index Backfile | 1932


    The N.A.C.A. variable-density wind tunnel

    Jacobs, Eastman N. / Abbott, Ira H. | TIBKAT | 1932