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有去旋进气共转盘腔内流动换热数值模拟
引用本文:陈阳春,王锁芳.有去旋进气共转盘腔内流动换热数值模拟[J].航空动力学报,2010,25(8):1746-1752.
作者姓名:陈阳春  王锁芳
作者单位:南京航空航天大学,能源与动力学院,南京,210016
摘    要:对左边转盘高位带去旋孔且附有内隔片的共转盘腔内的流动和换热进行了数值模拟.揭示了去旋角、旋转雷诺数、去旋喷嘴进气无量纲流量系数等参数对共转盘腔内的流动结构、压力损失和换热效果的影响.结果表明:盘腔内的总压降随无量纲流量系数的增加呈"S"形变化趋势;旋转雷诺数和冷气无量纲流量系数的增大都能增强转盘表面的换热效果;与预旋转静盘腔相比,去旋进气共转盘腔能使出口气流温度更低,冷却效果更好.

关 键 词:去旋  共转盘腔  流动换热  冷却效果  数值模拟
收稿时间:2009/6/26 0:00:00
修稿时间:2009/12/2 0:00:00

Numerical simulation of flow and heat transfer in the co-rotating cavity with de-swirl inflow
CHEN Yang-chun and WANG Suo-fang.Numerical simulation of flow and heat transfer in the co-rotating cavity with de-swirl inflow[J].Journal of Aerospace Power,2010,25(8):1746-1752.
Authors:CHEN Yang-chun and WANG Suo-fang
Institution:Nanjing University of Aeronautics and Astronautics
Abstract: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.
Keywords:de-swirl  co-rotating cavity  flow  heat transfer  numerical simulation
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