Wind tunnel static longitudinal stability and control characteristics of cruciform delta winged missile with various horizontal canards and trailing-edge flap control between Mach 1.50 and 4.63


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    Title :

    Longitudinal aerodynamic characteristics at Mach 1.50 to 4.63 of a missile model employing various canards and a trailing edge flap control


    Contributors:

    Publication date :

    1971-10-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :