A simulation model has been developed for use in piloted evaluations of takeoff, transition, hover, and landing characteristics of an advanced, short takeoff, vertical landing lift fan fighter aircraft. The flight/propulsion control system includes modes for several response types which are coupled to the aircraft's aerodynamic and propulsion system effectors through a control selector tailored to the lift fan propulsion system. Head-up display modes for approach and hover, tailored to their corresponding control modes are provided in the simulation. Propulsion system components modeled include a remote lift and a lift/cruise engine. Their static performance and dynamic response are represented by the model. A separate report describes the subsonic, power-off aerodynamics and jet induced aerodynamics in hover and forward flight, including ground effects.


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    Titel :

    Simulation Model of the Integrated Flight/Propulsion Control System, Displays, and Propulsion System for Astovl Lift-Fan Aircraft


    Beteiligte:
    W. Y. W. Chung (Autor:in) / P. F. Borchers (Autor:in) / J. A. Franklin (Autor:in)

    Erscheinungsdatum :

    1995


    Format / Umfang :

    51 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch







    ASTOVL Gas Coupled Lift Fan (GCLF) Propulsion System

    SAE / American Helicopter Society / AIAA | British Library Conference Proceedings | 1997


    ASTOVL Gas Coupled Lift Fan (GCLF) Propulsion System

    SAE / American Helicopter Society / AIAA | British Library Conference Proceedings | 1997