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带肋气膜冷却平板的数值模拟研究 被引量:4

NUMERICAL INVESTIGATION OF THE HEAT TRANSFER FOR A FILM COOLED FLAT PLATE
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摘要 本文对不带肋和带45°肋气膜冷却平板的三维对流换热与导热耦合传热问题进行了数值模拟。网格划分采用非结构化网格,湍流模型为SSTκ-ε模型,近壁处采用壁面函数法,采用SIMPLEC算法求解速度和压力的耦合。计算获得了不带肋和带45°肋气膜冷却平板的流场分布和平板内外表面的换热系数值。结果表明带45°肋的气膜冷却平板通道流场结构比较复杂,平板表面平均温度较无肋气膜冷却平板表面平均温度下降,而在近气膜孔区域冷、热表面平均换热系数较无肋时增大。 The flows and temperature field in internal film cooled flat plates with and without 45-deg ribs was investigated numerically. The finite volume method with unstructured meshes was used to solve the three dimensional compressible Navier-Stokes equations. The SST k - ω; turbulence model was used with the enhanced wall function for the near wall treatment. The velocity and pressure coupling used the SIMPLEC algorithm. The analysis produced the flow distributions and the heat transfer coefficients on the internal and external surfaces of the film cooled flat plate without and with 45-deg ribs. The numerical results show that the average surface temperatures of the hot and cold surfaces of the plate with the 45-deg ribs were lower than those without the ribs, the average heat transfer coefficients in the hot and cold surfaces near the film cooling holes of the plate with 45-deg ribs were higher than those without ribs.
作者 陆犇 姜培学
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2005年第5期844-846,共3页 Journal of Engineering Thermophysics
基金 国家杰出青年科学研究基金资助项目(No.50025617)
关键词 气膜冷却 温度 换热系数 数值模拟 film cooled rib temperature heat transfer coefficient numerical simulation
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参考文献5

  • 1Stephens M A, Shih T I-P, Civinskas K C. Computation of Flow and Heat Transfer in a Rectangular Channel with Ribs. In: 33rd Aerospace Sciences Meetings and Exhibit.AIAA-95-0180, 1995.
  • 2Yong-Jun Jang, Hamn-Ching Chen, Je-Chin Han. Flow and Heat Transfer in a Rotating Square Channel with 45 Deg Angled Ribs by Reynolds Stress Turbulence Model.Journal of Turbumachinery, 2001, 123(1): 124-132.
  • 3Chanteloup D, Bolcs A. Flow Characteristics in Two-Leg Internal Coolant Passage of Gas Turbine Airfoils With Fihn-Cooling Hole Ejection. Journal of Turbomachinery,2002, 124(7): 499-507.
  • 4倪萌,朱惠人,裘云,刘松龄.肋角度对流量系数影响的数值模拟研究[J].航空动力学报,2004,19(2):196-200. 被引量:19
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二级参考文献6

  • 1Chantetoup D,Bolcs A. Flow Characteristics in Two-Leg Internal Coolant Passages of Gas Turbine Airfoils With FilmCooling Hole Ejection[J]. Journal of Turbomachinery, 2002,124(7) :499-507.
  • 2FLUENT User's Guidep[M]. Fluent Inc. , Lebanon, NH,1999.
  • 3Stephens M A,Shih T I P, Civinskas K C. Computation of Flow and Heat Transfer in a Rectangular Channel with Ribs[R]. AIAA - 95 - 0180,33rd Aerospace Sciences Meetings and Exhibit.
  • 4Yong-Jun Jang, Hamn Ching Chen, Je-Chin Han. Flow and Heat Transfer in a Rotating Square Channel with 45 Deg Angled Ribs by Reynolds Stress Turbulence Model[J]. Journal of Turbomachinery, 2001,123(1 ): 124- 132.
  • 5Tong-Miin Liou, Meng-Yu Chen, Meng-Hsiun Tsai. Fluid Flow and Heat Transfer in a Rotating Two-Pass Square Duct with in Line 90-Deg Ribs [J]. Journal of Turbomachinery,2002,124 (4): 260- 268.
  • 6裘云,朱惠人,倪萌,刘松龄.带肋壁与出流孔内流通道中肋角度对流量系数的影响[J].航空动力学报,2003,18(2):235-238. 被引量:22

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