Combined flow control for corner separation in compressor cascades: A mechanistic and performance evaluation压气机叶栅中角区分离的复合流动控制:机理与性能评估AEROSPACE SCIENCE AND TECHNOLOGYIF5.82025-07-010PRE
Experimental and numerical research on combined design of corner separation in compressorAEROSPACE SCIENCE AND TECHNOLOGYIF5.82025-04-010PRE
Shock-dominated flow structures at the design condition of a supersonic through-flow fanPHYSICS OF FLUIDSIF4.32025-02-140PRE
Finely integrated design of end wall region for a compressor linear cascade through adjoint optimizationPHYSICS OF FLUIDSIF4.32025-01-240PRE
Vortex generator evaluation models and flow mechanisms for compressor cascadePHYSICS OF FLUIDSIF4.32024-11-140PRE
Experimental and numerical investigation of two blended blade and endwall configurationsCHINESE JOURNAL OF AERONAUTICSIF5.72024-09-011OAAI
Experimental and numerical research on blended blade and end wall technique in a compressor cascadePHYSICS OF FLUIDSIF4.32024-04-123PRE
Large eddy simulation and combined control of corner separation in a compressor cascadePHYSICS OF FLUIDSIF4.32022-07-0617PRE
Corner stall control in linear compressor cascade by blended blade and endwall technique based on large eddy simulationPHYSICS OF FLUIDSIF4.32021-11-1719PRE