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This paper presents numerical investigation on performance and flow field ofthe full-scale XV-15 tiltrotor in both helicopter mode (hovering flight andforward flight) and aeroplane propeller mode using Detached Eddy Simulation, inwhich the movement of the rotor is achieved using a Sliding Mesh Interface.Comparison of our CFD results against experiment data and other CFD results isperformed and presented.

Assessment of Detached Eddy Simulation and Sliding Mesh Interface in Predicting Tiltrotor Performance in Helicopter and Airplane Modes