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    Title :

    Propulsion/Airframe Integration Study for Ultra High Bypass Ratio Turbofan and a Slotted, Natural-Laminar-Flow Wing


    Contributors:

    Conference:

    AIAA SCITECH 2022 Forum



    Publication date :

    2022-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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