首页> 外文会议>American Society of Mechanical Engineers(ASME) Turbo Expo vol.3; 20040614-17; Vienna(AT) >EFFECTS OF DIMPLE DEPTH ON NUSSELT NUMBERS AND FRICTION FACTORS FOR INTERNAL COOLING IN A CHANNEL
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EFFECTS OF DIMPLE DEPTH ON NUSSELT NUMBERS AND FRICTION FACTORS FOR INTERNAL COOLING IN A CHANNEL

机译:通道深度对通道内冷却的小数值和摩擦系数的影响

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Experimental results, measured on dimpled test surfaces placed on one wall of different channels, are given for a ratio of air inlet stagnation temperature to surface temperature of approximately 0.94, and Reynolds numbers based on channel height from 9,940 to 74,800. The data presented include friction factors, local Nusselt numbers, spatially-averaged Nusselt numbers, and globally-averaged Nusselt numbers. The ratios of dimple depth to dimple print diameter δ/D are 0.1, 0.2, and 0.3 to provide information on the influences of dimple depth. The ratio of channel height to dimple print diameter is 1.00. At all Reynolds numbers considered, local and spatially-resolved Nusselt number augmentations increase as dimple depth increases (and all other experimental and geometric parameters are held approximately constant). These are attributed to: (ⅰ) increases in the strengths and intensity of vortices and associated secondary flows ejected from the dimples, as well as (ⅱ) increases in the magnitudes of three-dimensional turbulence production and turbulence transport. The effects of these phenomena are especially apparent in local Nusselt number ratio distributions measured just inside of the dimples, and just downstream of the downstream edges of the dimples. Data are also presented to illustrate the effects of Reynolds number, and streamwise development for δ/D = 0.1 dimples. Significant local Nusselt number ratio variations are observed at different streamwise locations, whereas variations with Reynolds number are mostly apparent on flat surfaces just downstream of individual dimples.
机译:在进气道停滞温度与表面温度之比约为0.94的情况下,给出了在放置于不同通道的壁上的凹陷测试表面上测得的实验结果,以及基于通道高度的雷诺数从9,940至74,800。呈现的数据包括摩擦系数,局部Nusselt数,空间平均Nusselt数和全局平均Nusselt数。凹痕深度与凹痕印刷直径δ/ D之比为0.1、0.2和0.3,以提供关于凹痕深度的影响的信息。通道高度与凹痕印刷直径的比率为1.00。在所有考虑的雷诺数下,随着酒窝深度的增加,局部和空间分辨的努塞尔特数增加都会增加(并且所有其他实验和几何参数都保持近似恒定)。这归因于:(ⅰ)涡流的强度和强度以及从酒窝喷出的相关二次流的强度增加,以及(ⅱ)三维湍流产生和湍流传输的幅度增加。这些现象的影响在酒窝内部和酒窝下游边缘下游的局部Nusselt数比分布中特别明显。还提供了数据以说明雷诺数的影响,以及δ/ D = 0.1酒窝的沿流方向发展。在不同的流向位置观察到明显的局部Nusselt数比变化,而雷诺数的变化在单个酒窝下游的平坦表面上最明显。

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