首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >EFFECT OF REYNOLDS NUMBER, HOLE PATTERNS AND HOLE INCLINATION ON COOLING PERFORMANCE OF AN IMPINGING JET ARRAY, PART Ⅰ: CONVECTIVE HEAT TRANSFER RESULTS AND OPTIMIZATION
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EFFECT OF REYNOLDS NUMBER, HOLE PATTERNS AND HOLE INCLINATION ON COOLING PERFORMANCE OF AN IMPINGING JET ARRAY, PART Ⅰ: CONVECTIVE HEAT TRANSFER RESULTS AND OPTIMIZATION

机译:雷诺数,孔图案和空穴倾斜对撞击喷射阵列的冷却性能的影响,第Ⅰ部分:对流传热结果和优化

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摘要

This study comprehensively illustrates the effect of Reynolds number, hole spacing, jet-to-target distance and hole inclination on the convective heat transfer performance of an impinging jet array. Highly resolved heat transfer coefficient distributions on the target plate are obtained utilizing transient liquid crystal over a range of Reynolds numbers varying between 5,000 and 25,000. Effect of streamwise and spanwise jet-to-jet spacing (X/D, Y/D: 4-8) and jet-to-target plate distance (Z/D: 0.75-3) are employed composing a test matrix of 36 different geometries. Additionally, the effect of hole inclination (0: 0°-40°) on the heat transfer coefficient is investigated. Optical hole spacing arrangements and impingement distance are pointed out to maximize the area-averaged Nusselt number and minimize the amount of cooling air. Also included is a new correlation, based on that of Florschuetz et al., to predict row-averaged Nusselt number. The new correlation is capable to cover low Z/D-0.75 and presents better prediction of row-averaged Nusselt number, which proves to be an effective impingement design tool.
机译:本研究全面地说明了雷诺数,孔间距,喷射目标距离和空穴倾斜对撞击喷射阵列的对流传热性能的影响。利用瞬态液晶在5,000至25,000之间的雷诺数范围内,获得靶板上的高度分辨的传热系数分布。使用流动和跨越射流间距(X / D,Y / D:4-8)和射流到目标板距离(Z / D:0.75-3)的效果组成36种不同的测试矩阵几何形状。另外,研究了空穴倾斜度(0:0°-40°)对传热系数的影响。光孔间隔布置和冲击距离被指出,以最大化面积平均的露珠数,并最小化冷却空气量。还包括基于Florschuetz等人的新相关性。,以预测行平均的纽带号。新相关能力能够覆盖低Z / D-0.75,并提高了行平均营销数的更好预测,这被证明是一种有效的冲击设计工具。

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