The ARL transonic wind tunnel is described. Originally built as a conventional subsonic high-speed tunnel it was converted in 1957 to transonic operation, and has been in operation since that time. It is a continuous flow, closed circuit tunnel with an electric drive system whose maximum power input is 2050 kW. The test section is 0.81 m high and 0.53 m wide. It is fitted with slotted walls and uses diffuser suction, covering a Mach number range of 0.4 to 1.4.


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    Titel :

    A.R.L. (Aeronautical Research Labs.) Transonic Wind Tunnel


    Beteiligte:
    J. B. Willis (Autor:in)

    Erscheinungsdatum :

    1982


    Format / Umfang :

    43 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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