Pitch and yaw characteristics of supersonic transport aircraft with variable sweep wings at various Mach numbers


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    Title :

    Aerodynamic Damping and Oscillatory Stability in Pitch and Yaw of a Variable-Sweep Supersonic Transport Configuration at Mach Numbers from 0.40 to 1.80


    Contributors:

    Publication date :

    1971-02-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :