Hypersonic wind tunnel (gun tunnel) at Institute for Aerodynamics of Deutsche Forschungsanstalt fuer Luft- und Raumfahrt (DFL): description of DFL gun tunnel and its operation; tunnel is equipped with hypersonic nozzle having variable throat section and exit diameter of 160 mm; Mach number range is from M 8 to M 15; stagnation temperatures ranging from 1400 to 2400 K are achieved and running times between 40 and 500 msec obtained: results of calibration and first model measurements.


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    Title :

    Die Hyperschall-Versuchsanlage (Gun-Tunnel) der Deutschen Forschungsanstalt fuer Luft- und Raumfahrt


    Additional title:

    Die Hyperschall-Versuchsanlage (Gun-Tunnel) der Deutschen Forschungsanstalt fuer Luft- und Raumfahrt


    Contributors:
    Gersten, G. (author) / Kausche, G. (author)

    Published in:

    Publication date :

    1966


    Size :

    13 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German


    Keywords :