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    Title :

    Tests of a Triangular Wing of Aspect Ratio 2 in the Ames 12-foot Pressure Wind Tunnel I : the Effect of Reynolds Number and Mach Number on the Aerodynamic Characteristics of the Wing with Flap Undeflected


    Contributors:

    Publication date :

    1948-01-22


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English