Wind tunnel of National Advisory Committee for Aeronautics is of the open-jet type with airstream 20 ft. in diam.; jet of air is drawn through open room; tunnel particularly suitable to testing airscrews; fan belt driven by Diesel engine; test chamber 50 by 60 ft. and 55 ft. high with traveling electric crane; new type of balance developed so that full sized fuselages might be tested. Abstract of N.A.C.A. Report No. 300.


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    Titel :

    N.A.C.A. 20 ft. propeller research tunnel


    Weitere Titelangaben:

    Aeroplane


    Beteiligte:
    Weick, F. (Autor:in) / Wood, D. (Autor:in)

    Erschienen in:

    Aeroplane ; 36 , n 17


    Erscheinungsdatum :

    1929


    Format / Umfang :

    4 pages


    Anmerkungen:

    3 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    N.A.C.A. High-speed wind tunnel and tests of six propeller sections

    Stack, J. | Engineering Index Backfile | 1933



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

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


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

    De France, S.J. | Engineering Index Backfile | 1933


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

    De France, Smith J. | TIBKAT | 1933