Effect of inlet radial distortion on aerodynamic stability in a multi-stage axial flow compressor

Jichao Li; Juan Du; Yang Liu; Hongwu Zhang; Chaoqun Nie

doi:10.1016/j.ast.2020.105886

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Effect of inlet radial distortion on aerodynamic stability in a multi-stage axial flow compressor

Jichao Li Juan Du Yang Liu Hongwu Zhang Chaoqun Nie

Year: 2020 Journal: Aerospace Science and Technology Vol: 105 Pages: 105886-105886 Publisher: Elsevier BV

DOI: 10.1016/j.ast.2020.105886

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Keywords:

Stall (fluid mechanics) Axial compressor Mechanics Inlet Tip clearance Casing Inflow Vortex Gas compressor Aerodynamics Secondary flow Flow separation Materials science Physics Boundary layer Engineering Aerospace engineering Mechanical engineering Turbulence

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Turbomachinery Performance and Optimization

Physical Sciences → Engineering → Aerospace Engineering

Heat Transfer Mechanisms

Physical Sciences → Engineering → Mechanical Engineering

Fluid Dynamics and Turbulent Flows

Physical Sciences → Engineering → Computational Mechanics

Effect of inlet radial distortion on aerodynamic stability in a multi-stage axial flow compressor

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