Numerical Simulation on Aerodynamic Characteristics of Transition Section of Tilt-Wing Aircraft
Qingjin Huang,
Guoyi He,
Jike Jia
et al.
Abstract:The tilt-wing aircraft has attracted widespread attention due to its excellent performance. However, its aerodynamic characteristics during the tilt transition section are characterized by unsteadiness, nonlinearity, and strong coupling, making it difficult to control. Using computational fluid dynamics (CFD) methods and moving overset grids to control the tilt-wing motion, the momentum source method is employed to replace actual propellers. The influence of the propeller on the aerodynamic characteristics of … Show more
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