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Turbomachinery Performance and OptimizationPlasma and Flow Control in AerodynamicsComputational Fluid Dynamics and Aerodynamics

Numerical Research on the Control of Shock-Induced Boundary Layer Separation in a Counter-Rotating Compressor Based on Blade Profile Curvature

Yongzhen Liu, Ben Zhao, Zhenghui Fan, Weiwei Cui, Qiang Zhou

2026.6.15Journal of Thermal Science

DOI: 10.1007/s11630-026-2306-7

Abstract

Abstract is not available.

Citation format

LIU, Yongzhen, et al. Numerical research on the control of shock-induced boundary layer separation in a counter-rotating compressor based on blade profile curvature. Journal of Thermal Science, 2026, 35(4): 1234–1245.