A high performance aircraft capable of subsonic, transonic and supersonic speeds employs a forward swept wing planform and at least one first-and-second-solution ejector located on the inboard section of the wing. A high degree of flow control on the inboard sections of the wing is achieved along with improved maneuverability and control of pitch, roll and yaw. Lift loss is delayed to higher angles of attack than in conventional aircraft. In one embodiment the ejectors may be advantageously positioned spanwise on the wing while the ductwork is kept to a minimum.


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    Titel :

    High Performance Forward Swept Wing Aircraft


    Beteiligte:
    D. G. Koenig (Autor:in) / K. Aoyagi (Autor:in) / M. E. Dudley (Autor:in) / S. B. Schmidt (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    27 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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