Consideration is given to the design phase of the highly maneuverable aircraft technology program. Design objectives are examined, noting full-scale design and the remotely piloted research vehicle. Attention is given to subsonic, transonic, and supersonic design. Design results are discussed with reference to aerodynamic efficiency, aeroelastic tailoring, and the flight test program.


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    Title :

    HiMAT aerodynamic design and flight test experience


    Contributors:

    Conference:

    Flight Testing Conference ; 1981 ; Las Vegas, NV


    Publication date :

    1981-11-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English