Numerical study on the effects of tip leakage flow distribution and intensity on stall margin in a transonic compressor rotor

Aerospace Science and Technology 2026

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Authors: Li Zeyuan, Wang Meng, Haimeng Zhou, Qu Yonglei, Wang Zhongyi

DOI: 10.1016/j.ast.2026.111654

Cited by: 1

References: 25

Fields of Study & Subjects

Turbomachinery Performance and Optimization Plasma and Flow Control in Aerodynamics Computational Fluid Dynamics and Aerodynamics

References 25