Short-duration test facility obtains extremely high Reynolds number flows in subsonic, transonic, and supersonic speed ranges, and aids in solving Reynolds number-dependent aerodynamic and thermodynamic problems in design and testing of large, high speed vehicles. The modified blowdown wind tunnel avoids data confusion and aerodynamic noise.


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    Title :

    Short-duration, transonic flow, variable-porosity test section


    Contributors:
    Davis, J. W. (author) / Hill, O. E. (author)

    Publication date :

    1970-09-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English