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    Study on aerodynamic characteristics of tilting wing unmanned aerial vehicle in transition state

    Study on aerodynamic characteristics of tilting wing unmanned aerial vehicle in transition state by MA Kai, LIN Changliang, PAN Minglong, WANG Xiong, LU Yang

    Published 2025-06-01

    In response to the problem of the continuous tilting transition process of the configuration of unmanned aerial vehicle with complex and unsteady aerodynamic characteristics, the real blade is replaced with a virtual propeller disk model, the rotor flow field is calculated by adding momentum source...

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