0000-0002-8472-6620 Employment
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Publications (10)
- Investigation of upstream wake effect on the endwall flow of a highly loaded compressor cascade at low Reynolds number Save
- Experimental and numerical investigation of passive flow control using L-shaped endwall groove in an axial flow compressor stage Save
- Numerical study on the effect of design parameters of circumferential multiple grooves on tip leakage flow reduction in a transonic turbine Save
- Review of unsteady aerodynamic problems and control strategies for the blade tip flow of axial compressors Save
- Numerical investigation into rotating instability and the vortex structure near the tip in a transonic compressor rotor Save
- The investigation on vortex breakdown prior to stall in a compressor rotor with non-uniform tip clearance Save
- Extraction of geometric features and analysis of flow mechanism of high loaded compressor airfoils at low Reynolds number Save
- Flow mechanism of a highly loaded low pressure turbine cascade with integrated-optimized end wall contouring and root lean Save
- Numerical study on effect of design parameters of the single-circumferential groove on tip leakage flow reduction in a transonic turbine Save
- The unsteadiness of tip leakage vortex breakdown and its role in rotating instability Save