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    Title :

    Effect of Several Tail Configurations on the Stability Characteristics of a Midwing Supersonic-Bomber Model at Mach Numbers of 1.60, 1.90, 2.20, AND 2.50


    Contributors:
    H. N. Silvers (author) / R. F. Wells (author)

    Publication date :

    1960


    Size :

    48 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English