The transonic wind tunnel Braunschweig is a pressurized blowdown windtunnel. The test section for two-dimensional airfoil testing has an area of 0.34 x 0.60 m. Mach number range is from 0.3 to 0.95 and Reynolds number range from 2,900,000 to 12 million at Mach 0.7, based on an airfoil chord length of 150 mm. Information required for the preliminary planning of test programs and for preliminary layout of models used in such programs is given.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Transonic Wind Tunnel (TWB) at DFVLR, Brunswick (Federal Republic of Germany)


    Contributors:

    Publication date :

    1987


    Size :

    47 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English