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ENDWALL HEAT TRANSFER MEASUREMENTS IN A STAGGERED PIN FIN ARRAY WITH AN ADIABATIC PIN

机译:具有绝热销的交错销翅片阵列的端壁传热测量

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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:使用红外相机在交错销翅片阵列中获取全表面端壁传热分布。基于引脚直径和通过相邻销的平均速度,在3000,10,000和30,000的雷诺数表示值。平均端壁篮板号码与每个雷诺数的档案值密切合法。局部平均的传热水平显示出通过前几行的入口的显着增加,最后是八行几何形状的下半部分的几乎流动的周期性状态。增加入口区域的传热水平可以归因于前沿涡流系统,围绕引脚的流动加速度以及湍流的产生。显示出湍流强度和湍流秤的分布,有助于通过阵列提取湍流运输条件。在前四个和最后四行的三个Reynolds数字上呈现并比较了详细的终止露珠编号分布。这些详细的传热分布突出了在销钉阵列中的入口区域和唤醒产生的湍流中的马蹄涡流系统的影响。局部速度和湍流分布与本地斯坦顿数和皮肤摩擦系数数据一起呈现,以检查湍流混合的侵略性。

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