Measurements of Effects of Finite Span on Pressure Distribution Over Double-Wedge Wings at Mach Numbers Near Shock Attachment.


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    Title :

    Measurements of effects of finite span on pressure distribution over double-wedge wings at mach numbers near shock attachment


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1955


    Size :

    50 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English