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西北工业大学 国内
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Effect of boundary layer suction on the corner separation in a highly loaded axial compressor cascade
Tian Liang,
Bo Liu
, Stephen Spence
动力与能源学院
Northwestern Polytechnical University Xian
Queen's University Belfast
科研成果
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同行评审
2
引用 (Scopus)
综述
指纹
指纹
探究 'Effect of boundary layer suction on the corner separation in a highly loaded axial compressor cascade' 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
Axial Compressors
100%
Blade Row
20%
Blade Span
20%
Boundary Layer
20%
Boundary Layer Suction
100%
Compressor Blade
20%
Compressor Efficiency
20%
Field Uniformity
20%
Flow Distribution
40%
Flow Rate
80%
Flow Separation
20%
Flow Velocity
80%
Loss Coefficient
20%
Pressure Gradient
20%
Pressure Loss Coefficient
20%
Separated Flow
20%
Suction Surface
100%
Turbomachinery
20%