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    Title :

    Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift


    Contributors:

    Publication date :

    1950-08-11


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English