Wing height effect on stability and control of 70 deg delta-wing canard-aircraft configuration at Mach 2.01


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    Title :

    Effects of wing height on the stability and control characteristics at a mach number of 2.01 of a canard airplane configuration with a 70 deg delta wing


    Contributors:
    Driver, C. (author)

    Publication date :

    1960-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English