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Keywords: rotor-stator interaction
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Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2025, 147(7): 071001.
Paper No: TURBO-24-1177
Published Online: November 22, 2024
...Yumeng Tang; Xindi Wei; Yangwei Liu Flows in compressors are extremely complex with various scales. Small-scale turbulence, middle-scale rotorstator interaction (RSI), large-scale corner separation, and tip leakage flow should all be considered in the simulation of compressors. Recently, a new...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. May 2025, 147(5): 051007.
Paper No: TURBO-24-1127
Published Online: November 12, 2024
... show that the periodic vortex shedding at the stator trailing edge emits strong pressure waves, and the upstream-propagating waves reflect against the adjacent stator suction surface. The POD modes related to the rotorstator interaction show peak amplitudes at the blade passing frequency and its...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. January 2024, 146(1): 011005.
Paper No: TURBO-23-1168
Published Online: October 25, 2023
... 10 2023 turbine stage turbulence rotorstator interaction unsteady-state mixing-plane clocking Grid Convergence Index computational fluid dynamics (CFD) fluid dynamics and heat transfer phenomena in compressor and turbine components of gas turbine engines The current energy...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2023, 145(7): 071004.
Paper No: TURBO-22-1301
Published Online: February 9, 2023
...Yangwei Liu; Xindi Wei; Yumeng Tang Unsteady blade row interaction (UBRI) has a large impact on performance in high-speed axial compressors. Thus, the influence of UBRI should be accurately predicted in compressor routine design. In this study, the unsteady rotorstator interaction in a transonic...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2008, 130(4): 041004.
Published Online: July 31, 2008
... profile pressure rotor-stator interaction tip clearance vortex wake negative jet effect wake–tip clearance vortex interaction A primary goal of the current compressor design is to increase the pressure ratio and the efficiency while reducing the number of blades and stages...