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    Title :

    Static and Dynamic-rotary Stability Derivatives of an Airplane Model with an Unswept Wing and a High Horizontal Tail at Mach Numbers of 2.5, 3.0, and 3.5


    Contributors:

    Publication date :

    1958-09-26


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English