首页> 外文会议>ASME(American Society of Mechanical Engineers) Turbo Expo vol.4 pt.A; 20070514-17; Montreal(CA) >ENDWALL HEAT TRANSFER MEASUREMENTS IN A STAGGERED PIN FIN ARRAY WITH AN ADIABATIC PIN
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ENDWALL HEAT TRANSFER MEASUREMENTS IN A STAGGERED PIN FIN ARRAY WITH AN ADIABATIC PIN

机译:带有绝热销的交错销翅片阵列中的端壁传热测量

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Full surface endwall heat transfer distributions have been acquired in a staggered pin fin array with the use of an infrared camera. Values are presented at Reynolds numbers of 3000, 10,000 and 30,000 based on pin diameter and average velocity through adjacent pins. Average endwall Nusselt numbers agree closely with archival values at each Reynolds number. Locally averaged heat transfer levels show a substantial increase from the inlet through the first few rows and finally a nearly streamwise periodic condition in the second half of the eight row geometry. Increasing levels of heat transfer in the inlet region can be attributed to the leading edge vortex system, flow acceleration around pins, and the generation of turbulence. Distributions of turbulence intensity and turbulent scale are shown to help document the turbulent transport conditions through the array. Detailed endwall Nusselt number distributions are presented and compared at the three Reynolds numbers for the first four and last four rows. These detailed heat transfer distributions highlight the influence of the horseshoe vortex system in the entrance region and the wake generated turbulence throughout the pin fin array. Local velocity and turbulence distributions are presented together with local Stanton number and skin friction coefficient data to examine the aggressive nature of the turbulent mixing.
机译:使用红外热像仪,可以在交错的针翅阵列中获得全部表面端壁传热分布。根据销直径和通过相邻销的平均速度,值以雷诺数3000、10,000和30,000表示。平均端壁Nusselt数与每个雷诺数的档案值非常吻合。局部平均的传热水平显示出从进口到前几排的热量显着增加,最后在八排几何的后半部分几乎呈流向周期性。入口区域传热水平的提高可归因于前缘涡流系统,销周围的流加速以及湍流的产生。示出了湍流强度和湍流尺度的分布,以帮助记录通过阵列的湍流传输条件。给出了详细的端壁Nusselt数分布,并比较了前四行和后四行的三个雷诺数。这些详细的传热分布突出了马蹄涡流系统在入口区域的影响以及尾流在整个针鳍阵列中产生的湍流。将局部速度和湍流分布与局部Stanton数和皮肤摩擦系数数据一起显示,以检查湍流混合的侵蚀性。

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