Several static and dynamic forced-motion wind tunnel tests have been conducted on a generic unmanned combat air vehicle (UCAV) configuration with a 53deg swept leading edge. These tests are part of an international research effort to assess and advance the state-of-art of computational fluid dynamics (CFD) methods to predict the static and dynamic stability and control characteristics for this type of configuration. This paper describes the dynamic forced motion data collected from two different models of this UCAV configuration as well as analysis of the control surface deflections on the dynamic forces and moments.


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    Title :

    Low-Speed Dynamic Wind Tunnel Test Analysis of a Generic 53 Degree Swept UCAV Configuration With Controls


    Contributors:

    Conference:

    AIAA Applied Aerodynamics Conference ; 2014 ; Atlanta, GA, United States
    AIAA Aviation and Aeronautics Forum and Exposition (AVIATION 2014) ; 2014 ; Atlanta, GA, United States


    Publication date :

    2014-06-16


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English