A wind-tunnel investigation was conducted with a vectored-thrust V/STOL fighter configuration. The model was equipped with two nacelle-mounted vectored-thrust jet simulators and one lift-jet simulator. The vectored-thrust jet could be tested at two alternate longitudinal positions and three nozzle deflection angles. The vectored-thrust configuration with the rear nozzles showed an increase in lift and a decrease in pitching moment when compared with the forward nozzles. The rear nozzles also improve stall characteristics. (Author)


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    Titel :

    Aerodynamic Characteristics of a Vectored-Thrust V/STOL Fighter in the Transition Speed Range


    Beteiligte:
    R. E. Mineck (Autor:in) / M. F. Schwendemann (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    181 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch