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S弯扩压器中四种湍流模型的比较

张丽芬 刘振侠 吕亚国

张丽芬, 刘振侠, 吕亚国. S弯扩压器中四种湍流模型的比较[J]. 航空动力学报, 2008, 23(10): 1888-1891.
引用本文: 张丽芬, 刘振侠, 吕亚国. S弯扩压器中四种湍流模型的比较[J]. 航空动力学报, 2008, 23(10): 1888-1891.
ZHANG Li-fen, LIU Zhen-xia, Lü Ya-guo. Comparison of four turbulence models in diffusing S-duct[J]. Journal of Aerospace Power, 2008, 23(10): 1888-1891.
Citation: ZHANG Li-fen, LIU Zhen-xia, Lü Ya-guo. Comparison of four turbulence models in diffusing S-duct[J]. Journal of Aerospace Power, 2008, 23(10): 1888-1891.

S弯扩压器中四种湍流模型的比较

Comparison of four turbulence models in diffusing S-duct

  • 摘要: 采用Realizableκ-ε,S-A(Spalart-Allmaras),SST(Shear stress transport剪切应力输运),RSM(Reynolds stress equation model雷诺应力模型)四种湍流模型对S弯扩压器内的分离流动进行了模拟,分析了不同湍流模型对计算结果的影响.将不同轴向位置的表面压力系数、分离区的大小、马赫数等三个量的实验值与计算值进行了比较,结果表明:分离区湍流模型对表面压力分布影响较大,未分离区不同湍流模型模拟精度相当;S-A模型对分离区的模拟较保守,RSM模型对分离的模拟精度较高,SST与RSM模拟结果很接近;各湍流模型计算的高速区域均比实验值大.扩压器的平均总压恢复系数受湍流模型影响不大,和实验结果吻合较好.

     

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出版历程
  • 收稿日期:  2007-10-15
  • 修回日期:  2008-02-20
  • 刊出日期:  2008-10-28

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