Effect of orifice shape in synthetic jet based impingement cooling

被引:125
|
作者
Chaudhari, Mangesh [1 ]
Puranik, Bhalchandra [1 ]
Agrawal, Amit [1 ]
机构
[1] Indian Inst Technol, Dept Mech Engn, Mumbai 400076, Maharashtra, India
关键词
Synthetic jet; Impinging flow; Cavity orifice shape; Impingement heat transfer; Electronics cooling; HEAT-TRANSFER DISTRIBUTION; SMOOTH FLAT SURFACE; AIR-JET; NOZZLE; GAS;
D O I
10.1016/j.expthermflusci.2009.11.001
中图分类号
O414.1 [热力学];
学科分类号
摘要
The effect of shape of the orifice of a synthetic jet assembly on impingement cooling of a heated surface is experimentally investigated in this study. The shapes considered are square, circular, and rectangular, of different aspect ratios (in the range of 1-20) and hydraulic diameters (3.8-8 mm). The average heat transfer coefficient as a function of the distance between the orifice and the heated surface is obtained. The Reynolds number (Re) is in the range of 950-4000 based on average velocity, while the normalized axial distance varies between 1 and 25. The heat transfer enhancement with a square orifice is found to be larger than that with rectangular and Circular shapes at larger axial distances z/d > 5, for the same set of boundary conditions. It is also found that rectangular orifice with aspect ratio between 3 and 5 gives best performance at smaller axial distances. An attempt is made to explain this behavior on phenomenological grounds. The effect of orifice shape on cooling with a synthetic jet is reported for the first time, and the present results are expected to have significant practical implications. (C) 2009 Elsevier Inc. All rights reserved.
引用
收藏
页码:246 / 256
页数:11
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