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Stator wake research in an axial-radial combined compressor with inlet distortion
Du Li, Dazhong Lao, Ben Zhao,
Ce Yang
机械与车辆学院
Beijing Institute of Technology
China Aviation Powerplant Research Institute
科研成果
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引用 (Scopus)
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探究 'Stator wake research in an axial-radial combined compressor with inlet distortion' 的科研主题。它们共同构成独一无二的指纹。
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Engineering
Axial Compressors
16%
Blade Surface
16%
Centrifugal
16%
Circumferential
33%
Combined Compressor
100%
Flow Characteristics
16%
Flow Loss
16%
Gradient Direction
16%
Multistage
16%
Navier-Stokes Equation
16%
Oscillation Characteristic
16%
Pressure Gradient
16%
Pressure Inlet
16%
Pressure Loss
16%
Pressure Pulsation
16%
Reynolds-Averaged Navier-Stokes
16%
Rotors
100%
Stage Compressor
16%
Turbocharger
16%