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Conjugate Heat Transfer from an Impingement and Film-Cooled Flat Plate

机译:从碰撞和薄膜冷却的平板上共轭传热

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摘要

The effect of solid thermal conductivity on conjugate heat transfer from a flat plate with combined impingement and film cooling is studied both experimentally and computationally. One side of the plate is exposed to hot mainstream, whereas the other side is impinged with air jets. A flow configuration with multiple staggered rows of cylindrical film holes and a matrix of impingement holes is considered. A thermochromic liquid crystal technique is used in the experiment to measure the surface temperature of the plate. The physical domain is meshed with fine-sized hybrid: hexahedral and tetrahedral grids suitable for the finite volume computations. Reynolds-averaged Navier-Stokes equations are solved with shear-stress transport κ-omega turbulence modeling. A grid independence study is carried out using a grid convergence index method. A validation exercise of computational results is carried out against the full coverage film cooling data available in literature ("Total Cooling Effectiveness on A Staggered Full-Coverage Film Cooling Plate with Impinging Jet," ASME-TurboExpo2010, American Soc. of Mechanical Engineers Paper GT2010-23725, Fairfield, NJ, June 2010). Results from the conjugate heat transfer study are presented for three blade materials: A, B, and C with thermal conductivities of 0.2,1.5, and 15 W/m · K, respectively, and for three blowing ratios of 0.6,1.0, and 1.6. Limited by the experimental facility, the mainstream Reynolds number is varied from 49,050 to 130,800; and the coolant jet Reynolds number is kept constant at 825. The computations for the impingement surface reveal multiple peaks and valleys in the heat flux and temperature plots. Material C has experienced significant changes in the values of impingement surface heat flux and temperature with blowing ratio, whereas these changes are only minor for material A. On the interaction surface, convective heat flux values are the lowest for material A and progressively increase with increasing thermal conductivity. However, the effectiveness values vary significantly for material A in the streamwise direction. A good agreement is found between the effectiveness distributions obtained from the measurements and the computations. The Nusselt number variations on the interaction surface are presented by defining a factor that accounts for the direction of heat flux.
机译:通过实验和计算研究了固体热导率对结合冲击和薄膜冷却的平板共轭传热的影响。板的一侧暴露于热主流下,而另一侧则受到空气射流的撞击。考虑具有多个交错排的圆柱状薄膜孔和冲击孔矩阵的流动配置。实验中使用热致变色液晶技术来测量板的表面温度。物理域与精细混合的网格啮合:适合于有限体积计算的六面体和四面体网格。雷诺平均的Navier-Stokes方程用切应力传输κ-ω湍流建模求解。使用网格收敛指数方法进行了网格独立性研究。针对文献中提供的全覆盖膜冷却数据(“具有冲击射流的交错式全覆盖膜冷却板的总冷却效率”,ASME-TurboExpo2010,美国机械工程师学会论文,GT2010)进行了计算结果的验证练习。 -23725,新泽西州费尔菲尔德,2010年6月)。共轭传热研究的结果分别针对三种叶片材料:A,B和C,其热导率分别为0.2、1.5和15 W / m·K,以及三种吹风比分别为0.6、1.0和1.6 。受实验设备的限制,雷诺的主流数量从49,050到130,800不等;冷却液射流的雷诺数保持恒定在825。撞击表面的计算显示出热通量和温度图中的多个峰和谷。材料C的冲击表面热通量和温度值随吹风比发生了显着变化,而这些变化仅对材料A较小。在相互作用表面上,对流热通量值对于材料A最低,并随温度的增加而逐渐增加导热系数。但是,材料A的效率值在流向上有很大变化。从测量和计算获得的有效性分布之间找到了很好的一致性。通过定义一个考虑热通量方向的因素,可以显示相互作用表面上的努塞尔数变化。

著录项

  • 来源
    《Journal of Thermophysics and Heat Transfer》 |2014年第4期|647-666|共20页
  • 作者单位

    Indian Institute of Technology Madras, 600 036 Chennai, India;

    Indian Institute of Technology Madras, 600 036 Chennai, India;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
  • 原文格式 PDF
  • 正文语种 eng
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