In order to investigate the flow and heat transfer performances in the co-rotating cavity with two inner shrouds and de-swirl inflow holes in its left disc
a numerical study was conducted.The effects of de-swirl angle
rotational Reynolds number and non-dimensional flow velocities on the flow and heat transfer characteristics in the co-rotating cavity were numerically simulated.The results show that the total pressure drop in the cavity exhibits an "S-curve" variation with the increase of non-dimensional mass flow coefficient.The heat transfer of the disc surface is enhanced with the increase of rotational Reynolds number and non-dimensional mass flow coefficient.The de-swirl inflow in the co-rotating cavity has better cooling efficiency than the pre-swirl inflow in the rotor-stator cavity.
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
Influence of tube length on flow resistance and temperature reduction characteristics of tubed vortex reducer
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
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