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    Title :

    Pressure coefficients at Mach numbers from 0.60 to 0.85 for a semispan wing with NACA 0012-64 section, 20-percent-chord plain aileron, and 0 degree and 45 degree sweepback


    Contributors:

    Publication date :

    1950-04-19


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English