1. Breakdown of tip leakage vortices in compressors at flow conditions close to stall;Schlechtriem,1997
2. The role of tip clearance in high-speed fan stall;Adamczyk;J. Turbomach.,1991
3. Effects of several porous casing treatments on stall limit and overall performance of an axial compressor rotor;Osborn,1971
4. Effect of grooved casing treatment on the flow range capability of a single-stage axial-flow compressor;Bailey,1972
5. Effect of circumferential grooves on the aerodynamic performance of an axial single-stage transonic compressor;Müller,2007