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    Title :

    NASA 5.2%-Scale Semispan High Lift Common Research Model Wind Tunnel Test at the 14- by 22-Foot Subsonic Tunnel


    Contributors:

    Conference:

    AIAA SCITECH 2025 Forum



    Publication date :

    2025-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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