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Influences of micro pin-fin on jet array impingement heat transfer: Effects of jet to target distance, micro pin-fin shapes, height, and Reynolds Number

机译:微型针状翅片对射流阵列撞击传热的影响:射流到目标距离,微型针状翅片形状,高度和雷诺数的影响

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In the current research of impingement on pin-fin wall, researchers mainly pay attention to macro pin-fin due to the limitation of manufacture. With the development of additive manufacturing, it is possible to manufacture the micro pin-fin. Hence, impingement on micro pin-fin wall becomes a new cooling technique that has attracted the researchers' attention. With experimental methodology , the investigation utilizes different jet to target distance, micro pin-fin shapes, height and Reynolds number for impingement cooling augmentation to illustrate the effects on jet array impingement heat transfer. The area-averaged target surface heat transfer coefficient distributions are measured with lumped capacitance method. The impingement hole diameter(D) is 4 millimeter, with streamwise and spanwise jet-to-jet spacing 4D. Considered are effects of jet to target plate distance(Z/D:0.75,3), micro pin-fin shapes(rectangle, pentahedron), and pin-fin height(h/D:0.05,0.2,0.4). In total, ten different test surfaces are considered(smooth surface included). Tests are performed at impingement jet Reynolds numbers from 2000 to 10000 for configuration of Z/D=0.75, from 5000-20000 for configuration of Z/D=3. The experimental results illustrate that there are significant heat transfer augmentation(30%-120% more than baseline flow condition) with micro pin-fin on impingement target surface, and discharge coefficient is almost the same.
机译:在目前对尖鳍墙体冲击的研究中,研究人员主要关注宏销鳍,由于制造的限制。随着添加剂制造的发展,可以制造微引脚翅片。因此,对微引脚墙的冲击成为一种新的冷却技术,吸引了研究人员的注意力。利用实验方法,调查利用不同的射流来瞄准距离,微引脚翅片形状,高度和雷诺数,用于冲击冷却增强,以说明对喷射阵列冲击传热的影响。通过集体电容法测量区域平均目标表面传热系数分布。冲击孔直径(d)是4毫米,具有流动和翼展的喷射到喷射间距4d。考虑是射流对靶板距离(Z / D:0.75,3),微引脚翅片形状(矩形,五边体)和尖翅(H / D:0.05,0.2,0.4)的效果。总共考虑十种不同的测试表面(包括光滑的表面)。从2000到10000的冲击喷射雷诺数进行测试,用于Z / D = 0.75的配置,从5000-20000配置Z / D = 3。实验结果表明,在冲击目标表面上具有显着的传热增强(30%-120%的基线流动条件),并且在冲击目标表面上具有微引脚翅片,并且放电系数几乎相同。

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