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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Contributors:
    Joshua Baculi (author) / Nhan Nguyen (author) / Wendy A. Okolo (author) / Juntao Xiong (author)

    Conference:

    AIAA Aviation Forum ; 2024 ; Las Vegas, NV, US


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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

    J. Baculi / N. Nguyen / W. A. Okolo et al. | NTIS | 2023


    Wake Vortex Interaction of Urban Air Mobility Aircraft

    Nguyen, Nhan T. / Bartolini, Graeson / Baculi, Joshua E. et al. | TIBKAT | 2022


    Wake Vortex Interaction of Urban Air Mobility Aircraft

    Nguyen, Nhan T. / Bartolini, Graeson / Baculi, Joshua E. et al. | AIAA | 2022


    Wake Vortex Effects Between Urban Air Mobility Aircraft

    Baculi, Joshua E. / Nguyen, Nhan T. / Okolo, Wendy et al. | AIAA | 2023


    Wake Vortex Effects Between Urban Air Mobility Aircraft

    Joshua Baculi / Nhan Nguyen / Wendy A. Okolo et al. | NTRS