The presentation describes supersonic flight testing accomplished on a novel mixed-compression axisymmetric inlet utilizing channels for off-design flow matching rather than a translating centerbody concept.


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    Title :

    Fundamental Aeronautics Program: Supersonics Project - Channeled Center-Body Inlet Experiment Overview


    Contributors:

    Conference:

    AIAA AV March Dinner Meeting ; 2012 ; Lancaster, CA, United States


    Publication date :

    2012-03-15


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English