0000-0002-9431-6668 Employment
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Publications (8)
- Reynolds number effect on the three-dimensional boundary layer separation-induced transition of compressors Save
- Aerodynamic data fusion for low-Reynolds-number compressors based on film-Re physics-guided multi-fidelity network Save
- Investigation on the stagger angle adjustment and loss mechanism of the supersonic through flow variable pitch tandem cascade Save
- Characteristics and flow mechanism of a transonic variable pitch fan Save
- Numerical investigations of vortex dynamics and loss generation in the corner separation region of a high subsonic compressor blade Save
- Numerical investigation of distributed roughness effects on separated flow transition over a highly loaded compressor blade Save
- Effects of Reynolds number and loading distribution on the aerodynamic performance of a high subsonic compressor airfoil Save
- Large eddy simulation of the separated flow transition on the suction surface of a high subsonic compressor airfoil Save