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• W3183298261 startingPage "110485" @default.
• W3183298261 abstract "An experimental investigation on the flow topology over a rotor operating at low Reynolds numbers is presented. The feasibility of laminar to turbulent transition experiments over small rotors is demonstrated. Phase-locked infrared thermography coupled with simultaneous force and torque measurements were used to study a three bladed rotor with a NACA0012 aerofoil section set at a uniform angle of incidence of 10°. Boundary layer transition was forced using two-dimensional (2D) and three-dimensional (3D) roughness elements, placed at approximately 5% and 28% of the rotor blades chord. In the 3D roughness configurations once the critical roughness Reynolds was attained the streaks downstream developed into fully turbulent wedges. For the current rotor configuration, it was found that the state of the boundary layer can significantly affect its performance, with the non-optimal forcing of laminar to turbulent transition generally resulting in a loss of performance when compared to the smooth reference rotor case." @default.
• W3183298261 created "2021-08-02" @default.
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• W3183298261 date "2022-01-01" @default.
• W3183298261 modified "2023-10-18" @default.
• W3183298261 title "Characterisation of boundary layer transition over a low Reynolds number rotor" @default.
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• W3183298261 doi "https://doi.org/10.1016/j.expthermflusci.2021.110485" @default.
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