The program objectives are: (1) Assess stability & control characteristics of a Blended Wing Body (BWB) class vehicle in free-flight conditions, (2) Assess flight control algorithms designed to provide desired flight characteristics, and (3) Evaluate prediction and test methods for BWB class vehicles.


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    Title :

    X-48B Blended Wing Body Ground to Flight Correlation Update


    Contributors:
    Vicroy, Dan (author)

    Conference:

    AIAA 2010 Conference ; 2011 ; Orlando, FL, United States


    Publication date :

    2011-01-04


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English






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