A study has been made to determine the aerodynamic characteristics of a low-aspect ratio cruciform missile model with all-movable wings and tails. The configuration was tested at Mach numbers from 1.50 to 4.63 with the wings in the vertical and horizontal planes and with the wings in a 45 deg roll plane with all-movable wings and tails. The configuration was tested at Mach numbers from 1.50 to 4.63 with the wings in the vertical and horizontal planes and with the wings in a 45 deg roll plane with tails in line and interdigitated. (Author)


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    Titel :

    Supersonic Aerodynamic Characteristics of a Low-Aspect-Ratio Missile Model with Wing and Tail Controls and with Tails in Line and Interdigitated


    Beteiligte:
    E. B. Graves (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    274 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch