Pressure distribution measurements on semi-span rectangular wing model.


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    Title :

    Flow about section of finite-aspect-ratio NACA-0018 airfoil on transonic bump


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1953


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English