An experimental investigation has been conducted to evaluate a unique engine-over-wing propulsive-life scheme for providing maneuver improvement in the subsonic-transonic speed regime. The concept combines the benefits of vectored thrust for added circulation and spanwise blowing for leading-edge-vortex augmentation so as to provide full angle-of-attack aerodynamic improvements. Results of a series of wind tunnel tests employing a powered research model illustrate the propulsive/aerodynamic features of the concept.


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    Titel :

    A vectored-engine-over-wing propulsive-lift concept


    Beteiligte:
    Bradley, R. G. (Autor:in) / Jeffries, R. R. (Autor:in) / Capone, F. J. (Autor:in)

    Erscheinungsdatum :

    01.09.1976


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





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