For exploring the beneficial usage of profiled endwall on axial flow compressors.A profiled endwall was designed and numerically studied on a subsonic axial flow compressor stage of Northwest Polytechinical University was numerically studied.According to the nature of the adverse pressure gradient working environment of compressors
the contouring of the stator endwall was conducted on both streamwise and circumferential directions.Detailed design method was introduced in the paper.Research of this paper shows that: endwall contouring can effectively reduce the stator hub corner separation
and consequently improve the compressor pressure ratio and working efficiency.
Response of an Transonic Two-Stage Compressor to Steady Circumferential Total Pressure Distortions
Simulation method of short crack propagation in turbine disks based on crystal plasticity
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Impact of Reynolds number on unsteady flow in axial flow compressor rotor
Numerical simulation of light-craft effects onlaser supported donation wave with gas-liquid two phase propellant
Related Author
WU Hu
JIA Hai-jun
HUANG Jian
Ping ZHANG
Shan LU
Xin JING
Mao YANG
Zhongbing LUO
Related Institution
School of Power and Energy, Northwestern Polytechnical University
School of Power and Energy,Northwestern Polytechnical University
Nondestructive Testing and Evaluation Laboratory, Dalian University of Technology
College of Civil Engineering, Hefei University of Technology
Key Laboratory of Aerospace Chemical Power Technology, Hubei Institute of Aerospace Chemical Techologh, China Aerospace Science and Technology Corporation,Xiangyang Hubei