The Langley 16-foot transonic tunnel with test section air removal (plenum suction) was calibrated to a Mach number of 1.3. The results of the calibration, including the effects of slot shape modifications, test section wall divergence, and water vapor condensation, are presented. A complete description of the wind tunnel and its auxiliary equipment is included. (Author)


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    Titel :

    Calibration of the Langley 16-Foot Transonic Tunnel with Test Section Air Removal


    Beteiligte:
    B. W. Corson (Autor:in) / J. F. Runckel (Autor:in) / W. B. Igoe (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    118 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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