The NUMECA software Fine/Turbo is employed to investigate the three dimensional viscous flow in a diagonal fan impeller at the operating conditions with and without blade tip clearance respectively.The limiting streamlines
secondary flow patterns and velocity distributions of the two flow fields are analyzed by comparison between their numerical and experimental results.The transportation of low energy fluid in the flow passage
"jet/wake" structure and the formation of tip leakage vortex are revealed.The results show that the non-uniform flow wake induced by secondary motion and vortex always appear in the corner region of casing wall and pressure surface;and the effects of the tip clearance are to reduce the efficiency of the impeller and to enlarge the non-uniform level of the outflow field in the impeller.
Simulation method of short crack propagation in turbine disks based on crystal plasticity
Numerical simulation of internal flow field in gas generator of fire extinguishing bomb
Numerical simulation of light-craft effects onlaser supported donation wave with gas-liquid two phase propellant
Flow field in and near the open-end swirl injector
Low-Reynolds-number wake flows of a triangular prism
Related Author
Ping ZHANG
Shan LU
Xin JING
Mao YANG
Zhongbing LUO
Rongxin ZHOU
Yunfeng LI
Kangqing DENG
Related Institution
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
Hubei Institute of Aerospace Chemistry Technology, China Aerospace Science and Technology Corporation,Xiangyang Hubei