Numerical investigations on the key contributing factor and flow features of compressor stall hysteresis

Aerospace Science and Technology - Tập 121 - Trang 107306 - 2022
Zhiping Li1,2,3, Peng Zhang4, Dong Yang1,2,3, Jian Zhang3
1National Key Laboratory of Science and Technology on Aero-Engine Thermodynamics, Beihang University, Beijing 100083, China
2Collaborative Innovation Center for Advanced Aero-Engine, Beihang University, Beijing 100083, China
3School of Energy and Power Engineering, Beihang University, Beijing 100083, China
4College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, China

Tài liệu tham khảo

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