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应用各向异性湍流模型对气膜冷却的数值研究
引用本文:朱剑琴,徐国强,孙纪宁,邓宏武.应用各向异性湍流模型对气膜冷却的数值研究[J].航空动力学报,2010,25(4):761-767.
作者姓名:朱剑琴  徐国强  孙纪宁  邓宏武
作者单位:北京航空航天大学 能源与动力工程学院 航空发动机气动热力科技重点实验室, 北京 100191
摘    要:应用引入各向异性系数的k-w湍流模型和标准k-ε模型,对平板气膜冷却经典实验进行了数值研究,分析了各向异性系数的引入对气膜孔下游流场与温度场的影响机理,探讨了该系数的适用性问题.研究表明:①展向各向异性系数的引入,增加了流体在展向的湍流脉动,强化了气膜冷气沿展向的扩散;②各向异性模型的计算结果在低吹风比(M=0.5)的工况下与实验值符合得较好;③各向异性系数在气膜脱离壁面与主流掺混的区域适用性较差. 

关 键 词:气膜冷却    数值模拟    各向异性    湍流模型    冷却效率
收稿时间:4/8/2009 10:15:14 AM
修稿时间:9/2/2009 12:00:00 AM

Numerical investigation of film cooling with anisotropic turbulence model
ZHU Jian-qin,XU Guo-qiang,SUN Ji-ning and DENG Hong-wu.Numerical investigation of film cooling with anisotropic turbulence model[J].Journal of Aerospace Power,2010,25(4):761-767.
Authors:ZHU Jian-qin  XU Guo-qiang  SUN Ji-ning and DENG Hong-wu
Institution:National Key Laboratory of Science and Technology on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
Abstract:An in-house three-dimensional Navier-Stokes code was developed to evaluate numerically the advantages of the anisotropic turbulence model over the classical isotropic k-ε model in a typical film cooling experiment. The anisotropic turbulence model was the k-ω turbulence model incorporated with anisotropic coefficient. The effects of the anisotropic tur-bulent transport coefficient on the flow and temperature filed were analyzed in detail. The applicability of this model was also discussed. Comparison result reveals that the introduc-tion of the anisotropic turbulent transport coefficient intensified the turbulent mixing of cool-ing jet with the main stream in lateral direction, and subsequently enhanced the lateral sprea-ding of cooling air. The cooling effectiveness in centerline predicted by the anisotropic model was much closer to experimental data than that by the standard k-ε model. The anisotropic model was in good agreement with the experimental results at low-mass flux ratio condition (M=0.5). However, with the increase of mass flux ratio, the jets tend to be detached and then reattached to the wall, the discrepancy upstream the reattachment increased due to the limitation of the anisotropic coefficient, and downstream the reattachment these two agreed well consistently.
Keywords:film cooling  numerical investigation  anisotropy  turbulence model  cooling effectiveness
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