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    Title :

    Test Summary of the NASA High-Lift Common Research Model Half-Span at QinetiQ 5-Metre Pressurized Low-Speed Wind Tunnel


    Contributors:

    Conference:

    AIAA AVIATION 2020 FORUM



    Publication date :

    2020-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English





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