An investigation has been made to determine the effects of the location of the wing pivot and geometry of the forewing on the static longitudinal aerodynamic characteristics at subsonic speeds of a model representing a variable-sweep supersonic fighter airplane. Results indicate that as the wing-pivot location moves aft and outboard, the change in static margin due to wing sweep is reduced. Increasing the forewing area resulted in a forward shift of the aerodynamic center as well as a slight reduction in the aerodynamic-center variation due to wing sweep. (Author)


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    Titel :

    Effects of Wing-Pivot Location and Forewing Configuration on the Low-Speed Aerodynamic Characteristics of a Variable-Sweep Airplane Model


    Beteiligte:
    J. K. Huffman (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    58 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch