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.


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    Title :

    Calibration of the Langley 16-foot transonic tunnel with test section air removal


    Contributors:

    Publication date :

    1974-08-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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