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    Title :

    An Investigation of the Effects of Jet Exhaust and Reynolds Number upon the Flow over the Vertical Stabilizer and Rudder of the Douglas D-558-II Research Airplane at Mach Numbers of 1.62, 1.93, and 2.41


    Contributors:

    Publication date :

    1954-06-17


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English