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    Title :

    Longitudinal and Lateral Stability and Control Characteristics at Mach Number 2.01 of a 60 Degree Delta-wing Airplane Configuration Equipped with a Canard Control and with Wing Trailing-edge Flap Controls


    Contributors:

    Publication date :

    1958-03-10


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English