The flow inside an enclosed rotor-stator disc cavity was studied numerically.The disc cavity was composed of a rotating disc
a stationary disc and a stationary shroud.The standard k-ε turbulence model was employed in the core region of the cavity.Two low Reynolds number turbulence models
single equation model and Launder-Sharma Low Reynolds number k-ε model
were used in the near wall region.The modification of dissipation rate decrease caused by solid body rotation was considered in the second model.The results showed that Launder-Sharma low Reynolds k-ε model could more accurately reproduce the experimental data than the single equation model.
Numerical methods in simulation of annular combustor cold flow field
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
Low-Reynolds-number wake flows of a triangular prism
Related Author
CAI Wen-xiang
ZHAO Jian-xing
HU Hao-sheng
WU Xiao-song
Ping ZHANG
Shan LU
Xin JING
Mao YANG
Related Institution
School of Mechanical Engineering,Nanjing University of Science and Technology
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