首页> 外文期刊>Experimental Heat Transfer >INFLUENCE OF STREAMWISE PITCH ON LOCAL HEAT TRANSFER DISTRIBUTION FOR IN-LINE ARRAYS OF CIRCULAR JETS WITH SPENT AIR FLOW IN TWO OPPOSITE DIRECTIONS
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INFLUENCE OF STREAMWISE PITCH ON LOCAL HEAT TRANSFER DISTRIBUTION FOR IN-LINE ARRAYS OF CIRCULAR JETS WITH SPENT AIR FLOW IN TWO OPPOSITE DIRECTIONS

机译:方向间距对两个方向有气流的圆形射流直列阵列的局部传热分布的影响

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The effect of streamwise jet-to-jet spacing on local heat transfer distribution due to an inline rectangular array of confined multiple circular air jets impinging on a surface parallel to the jet plate are experimentally studied. The length-to-diameter ratio of nozzles of the jet plate is 1.0. The flow, after impingement, is constrained to exit in two opposite directions from the confined passage formed between the jet plate and target plate. Mean jet Reynolds numbers based on the nozzle exit diameter (d) covered are 3,000, 5,000, 7,500, and 10,000; jet-to-plate distances studied are d, 2d, and 3d. Streamwise jet-to-jet distances of 3d, 4d, and 5d, and a constant spanwise pitch of 4d, are considered. The jet plates have ten spanwise rows in the streamwise direction and six jets in each spanwise row. The fiat heat transfer surface is made of thin stainless-steel metal foil. Local temperature distribution on a target plate is measured using a thermal infrared camera. Wall static pressures in the streamwise direction are measured midway between the spanwise jets to estimate cross-flow velocities and individual jet velocities. The streamwise distribution of the jet flow and the cross flow is found to be least influenced by the streamwise pitch variation for the range of parameters considered during the present study. Heat transfer characteristics are explained partially on the basis of flow distribution. The cooling performance, based on the strip-averaged Nusselt number per unit mass flow rate of coolant per unit area of cooled surface, indicates deterioration for lower streamwise pitch and higher jet-to-plate distance.
机译:实验研究了由于有限的多个圆形空气射流的直列矩形阵列撞击平行于射流板的表面而导致的射流到射流间距对局部传热分布的影响。喷射板的喷嘴的长径比为1.0。撞击后,气流被限制在两个相反的方向从射流板和目标板之间形成的受限通道中流出。基于所覆盖的喷嘴出口直径(d)的平均雷诺数为3,000、5,000、7,500和10,000;研究的射流到板的距离分别是d,2d和3d。考虑了3d,4d和5d的沿流方向的喷射距离,以及恒定的跨度间距4d。射流板在流方向上具有十个翼展方向行,并且在每个翼展方向行中具有六个射流。平板传热表面由薄的不锈钢金属箔制成。使用红外热像仪测量目标板上的局部温度分布。在翼展方向射流之间的中途测量沿流向的壁静压力,以估计横流速度和各个射流速度。在本研究中考虑的参数范围内,发现射流和错流的沿河方向分布受流向螺距变化的影响最小。根据流动分布部分地解释了传热特性。基于每单位冷却表面每单位面积冷却剂的质量平均流速的条带平均努塞尔数,其冷却性能表明,沿较低的流向节距和较高的射流到印版距离会变差。

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