This study continues previous research evaluating the aircraft flight dynamics in the presence of wake disturbances. A model for fixed-wing-generated wake effects is input to the closed-loop system of a Revolutionary Vertical Lift Technology (RVLT) Lift+Cruise aircraft operating in the fixed-wing Cruise configuration. The wake effects are implemented as a time-varying nonlinear aerodynamic model that affect the stability, dynamic, and control derivatives of the aircraft at every time step. The final product of this study is a reduced separation minimum based on further simulation testing with the nonlinear RVLT Lift+Cruise aircraft model, as well as additional wake inputs from rotorcraft and static urban canyons.


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    Titel :

    Wake Disturbance-Based Separation Criteria Study for Urban Air Mobility Aircraft


    Beteiligte:
    J. Baculi (Autor:in) / N. Nguyen (Autor:in) / W. A. Okolo (Autor:in) / J. Xiong (Autor:in)

    Erscheinungsdatum :

    2023


    Format / Umfang :

    13 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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