This paper documents the control laws used in the free-flight tests of a 5% scaled blended-wing-body aircraft in the NASA Langley 30x60 Full-Scale Tunnel, conducted in the summer of 2005.


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    Title :

    Control Laws for a Wind Tunnel Free-Flight Study of a Blended-Wing-Body Aircraft


    Contributors:

    Publication date :

    2006-08-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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