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西北工业大学 国内
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Mechanism of unsteady influence of tip injection on a high-loaded axial compressor performance
Wei Wang,
Wu Li Chu
,
Hao Guang Zhang
动力与能源学院
Northwestern Polytechnical University Xian
Collaborative Innovation Center for Advanced Aero-Engine
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期刊稿件
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引用 (Scopus)
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探究 'Mechanism of unsteady influence of tip injection on a high-loaded axial compressor performance' 的科研主题。它们共同构成独一无二的指纹。
分类
加权
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Engineering
Blade Passage
100%
Axial Compressors
100%
Compressor Performance
100%
Blade Tip
66%
Circumferential
33%
Flow Distribution
33%
Trailing Edge
33%
Pressure Ratio
33%
Aerodynamic Performance
33%
Stability Margin
33%
Compressor Efficiency
33%
Aerodynamic Stability
33%
Compressor Inlet
33%