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    Title :

    Computational Evaluation of Inlet Distortion on an Ejector Powered Hybrid Wing Body at Takeoff and Landing Conditions (Invited) (AIAA 2016-0264)



    Conference:

    Aerospace sciences meeting



    Publication date :

    2016-01-01


    Size :

    21 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English