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    Title :

    Wind-Tunnel Investigation at a Mach Number of 2.01 of the Aerodynamic Characteristics in Combined Angles of Attack and Sideslip of Several Hypersonic Missile Configurations with Various Canard Controls


    Contributors:

    Publication date :

    1958


    Size :

    35 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English