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Wake Disturbance-Based Separation Criteria Study for Urban Air Mobility Aircraft.
| 题名： | Wake Disturbance-Based Separation Criteria Study for Urban Air Mobility Aircraft. |
| 作者： | Baculi, J; Nguyen, N; Okolo, W. A; Xiong, J. |
| 摘要： | 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. |
| 总页数： | 13 pages |
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