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Heat transfer and fluid flow characteristics of a turbulent wall jet with a wavy wall

机译:湍流壁射流的传热和流体流动特性用波浪壁

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The fluid flow and heat transfer characteristics of a turbulent wavy wall jet have been studied numerically using the low Reynolds number model. The three low Reynolds number models, Realizable, RNG and SST are used for code validation with the experimental results present in the literature for the plane wall jet. The best suited model is used further to study the wavy wall jet. The sinusoidal profile (y = amplitude * sin(2 pi N/l x) has been used for the wavy wall, where N is total number of cycles and l is total length of wavy wall. In order to study the influence of amplitude on heat transfer and flow behavior, the wavy wall amplitude has been changed from 0 (plane wall) to 0.8 at an interval of 0.1 and number of cycles kept 10 for all the cases. The Reynolds number of heated jet is kept 15000 by using a slot nozzle of height 20 mm and exit velocity 10.95 m/s. The flow separation and re-circulation zone are studied with the help of pressure gradient (dP/dX) and streamwise velocity gradient (dU/dY) for each case. The results show that the flow remains attached till 0.3 amplitude after that flow gets separated. It is found that for amplitude 0.4, 0.5, 0.6, 0.7 and 0.8, separation starts for the first time at X = 56.4, X = 41, X = 26.3, X = 25.9 and X = 25.5. The area of re-circulation zone is found to increase as the amplitude of wavy surface increases from 0.4 to 0.8. Also, the maximum streamwise velocity is found to increase with the increase in the amplitude of the wavy wall. These characteristics influenced the average Nusselt number drastically. The average Nusselt number is on the higher side as compared to the case of a plane wall. However, the trend is not monotonic; it increases till amplitude 0.7 and then it decreases. A maximum increase of 19.08% is observed for the wavy wall with amplitude 0.7. The thermal hydraulic performance (THP) is increased by 5.3% for amplitude 0.8 with respect to plane wall jet.
机译:使用低雷诺数模型在数值上进行了数量地研究了湍流波浪壁射流的流体流动和传热特性。三个低雷诺数模型,可实现的,RNG和SST用于代码验证,该代码验证与平面壁射流的文献中存在的实验结果。最适合的模型用于进一步用于研究波浪壁射流。正弦轮廓(Y =幅度* SIN(2 PI N / LX)已用于波状壁,其中N是循环的总数,L是波浪墙的总长度。为了研究幅度对热量的影响转移和流动行为,波浪壁幅度以0.1的间隔从0(平面壁)变为0.8,并且所有情况下保持10的循环数量。通过使用槽喷嘴保持15000的雷诺数。高20 mm和出口速度10.95 m / s。对于每种情况的压力梯度(dp / dx)和流动速度梯度(du / dy)研究流动分离和再循环区。结果表明在流动分离后,流动保持直到0.3幅度。发现,对于幅度0.4,0.5,0.6,0.7和0.8,分离在x = 56.4,x = 41,x = 26.3时首次开始分离。 25.9和x = 25.5。发现重新循环区的区域随着波浪表面的幅度从0增加而增加.4至0.8。而且,发现最大流速随着波浪墙的幅度的增加而增加。这些特征急剧影响了平均水果数量。与平面墙的情况相比,平均纽带数在较高侧。但是,这种趋势不是单调;它增加到幅度0.7,然后减少。对于具有幅度0.7的波浪壁,观察到最大增加19.08%。对于平面壁射流,热液压性能(THP)增加了0.8的幅度0.8的5.3%。

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