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直接供气预旋转静系流动和换热数值模拟

罗翔 冯野 徐国强 赵熙 赵南

罗翔, 冯野, 徐国强, 赵熙, 赵南. 直接供气预旋转静系流动和换热数值模拟[J]. 航空动力学报, 2012, 27(10): 2188-2193.
引用本文: 罗翔, 冯野, 徐国强, 赵熙, 赵南. 直接供气预旋转静系流动和换热数值模拟[J]. 航空动力学报, 2012, 27(10): 2188-2193.
LUO Xiang, FENG Ye, XU Guo-qiang, ZHAO Xi, ZHAO Nan. Numerical simulation of flow and heat transfer performances in a direct transfer pre-swirl system[J]. Journal of Aerospace Power, 2012, 27(10): 2188-2193.
Citation: LUO Xiang, FENG Ye, XU Guo-qiang, ZHAO Xi, ZHAO Nan. Numerical simulation of flow and heat transfer performances in a direct transfer pre-swirl system[J]. Journal of Aerospace Power, 2012, 27(10): 2188-2193.

直接供气预旋转静系流动和换热数值模拟

Numerical simulation of flow and heat transfer performances in a direct transfer pre-swirl system

  • 摘要: 采用CFD商业软件FLUENT分别从维度模型和湍流模型两个角度对接近真实的高压涡轮旋转盘腔进行数值模拟,研究了一种直接供气预旋转静系旋转盘腔模型内的流动和换热特性.通过计算研究发现:低位腔内的流动仅由中心入流控制,二维计算不能反映高位腔内中心入流与预旋入流的掺混;二维和三维计算所得的腔内压力分布相似,实验值介于两者之间;主盘面的换热主要受中心入流控制,二维和三维计算差别不大,Realizable k-ε湍流模型在定性和定量上均能更好地反映换热实验结果.

     

  • [1] Karabay H,Chen J X,Pilbrow R.Flow in a cover-plate preswirl rotor-stator system[J].Transactions of the ASME,1999,121(1):160-166.
    [2] Karabay H,Pilbrow R,Wilson M.Performance of pre-swirl rotating-disc systems[J].Transactions of the ASME,2000,122(3):442-450.
    [3] Karabay H,Wilson M,Owen J M.Approximate solutions for flow and heat transfer in pre-swirl rotating-disc systems .AMSE Paper 2001-GT-0200,2001.
    [4] Yan Y,Farzaneh-Gord M,Lock G D,et al.Fluid dynamics of a pre-swirl rotor-stator system[J].Journal of turbomachinery,2003,125(4):641-647.
    [5] Farzaneh-Gord M,Wilson M,Owen J M.Numerical and theoretical study of flow and heat transfer in a pre-swirl rotor-stator system .ASME Paper GT2005-6813,2005.
    [6] Lewis P W,Wilson M,Lock G.Physical interpretation of flow and heat transfer in pre-swirl systems[J].Journal of Engineering for Gas Turbines and Power,2007,129(3):769-778.
    [7] Schneider O,Dohmen H J,Benra F K.Analysis of dust separation inside a pre-swirl cooling air system .ISROMAC10-2004-029,2004.
    [8] Schneider O,Dohmen H J,Benra F K.Investigations of dust separation in the internal cooling air system of gas turbines .ASME Paper GT2003-38293,2003.
    [9] Jarzombek K,Dohmen H J,Benra F K. Flow analysis in gas turbine pre-swirl cooling air systems:variation of geometric parameters .ASME Paper GT2006-90445,2006.
    [10] 丁水汀,陶智,徐国强.带进气预旋的旋转空腔平均换热特性研究[J].航空动力学报,1998,13(3):277-280. DING Shuiting,TAO Zhi,XU Guoqing.A study on averaged heat transfer characteristics of a rotating cavity with preswirling inflow[J].Journal of Aerospace Power,1998,13(3):277-280.(in Chinese)
    [11] 丁水汀,徐国强,陶智.外缘预旋进气的旋转空腔主盘局部换热及流阻特性研究[J].推进技术,1998,19(6):45-49. DING Shuiting,XU Guoqing,TAO Zhi.Local heat transfer and flow characteristics of rotating cavity with tangential pre-swirling fringe guide van and radial outlet[J].Journal of Propulsion Technology,1998,19(6):45-49.(in Chiese)
    [12] 罗翔,徐国强,陶智.30°预旋进气旋转盘流动与换热特性的实验[J]. 北京航空航天大学学报,2007,33(3):290-293. LUO Xiang,XU Guoqing,TAO Zhi.Flow and heat transfer in rotor-stator system with pre-swirl angle of 30°[J].Journal of Beijing University of Aeronautics and Astronautics,2007,33(3):290-293.(in Chiese)
    [13] 罗翔,徐国强,陶智.进气角度对旋转盘冷却效果的影响[J].推进技术,2007,28(3):240-244. LUO Xiang,XU Guoqing,TAO Zhi.Cooling effectiveness in a rotor-stator system with different pre-swirl angles[J].Journal of Propulsion Technology,2007,28(3):240-244.(in Chinese)
    [14] 丁水汀,李烨,张弓.旋转盘腔预旋角度的敏感性分析[J].航空动力学报,2011,26(10):2251-2257. DING Shuiting,LI Ye,ZHANG Gong.Sensibility analysis of inlet pre-swirl angle in the rotating cavity[J].Journal of Aerospace Power,2011,26(10):2251-2257.(in Chinese)
    [15] 陈懋章.粘性流体动力学基础[M].北京:高等教育出版社,2002.
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出版历程
  • 收稿日期:  2012-01-16
  • 刊出日期:  2012-10-28

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