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西北工业大学 国内
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Test of unsteady flow in the tip clearance of low speed axial flow compressor
Limin Gao
, Yongzeng Li, Xiaodong Liu, Shuai Zhang
动力与能源学院
Collaborative Innovation Center for Advanced Aero-Engine
Northwestern Polytechnical University Xian
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Engineering
Adjacent Channel
33%
Axial Compressors
33%
Axial-Flow Compressors
100%
Blade Tip
66%
Characteristic Frequency
33%
Chord Length
33%
Circumferential Direction
66%
Compressor Rotor
33%
Dynamic Pressure
33%
Flow Distribution
33%
Leading Edge
100%
Leakage Flow
66%
Pressure Fluctuation
33%
Pressure Sensor
33%
Rotor Speed
33%
Rotors
33%
Stall Cell
66%
Trailing Edge
33%
Unsteady Flow
100%
Waveform
33%