A fan-driven transonic cryogenic tunnel was designed, and its purging, cooldown, and warmup times were determined satisfactory. Cooling with liquid nitrogen is at the power levels required for transonic testing. Good temperature distributions are obtained by using a simple nitrogen injection system. (Author)


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    Titel :

    Design Features and Operational Characteristics of the Langley Pilot Transonic Cryogenic Tunnel


    Beteiligte:
    R. A. Kilgore (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    61 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch