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MODELLING OF THE OPPOSING MIXED CONVECTION HEAT TRANSFER IN A ONE-SIDE HEATED VERTICAL FLAT CHANNEL IN THE TRANSITION REGION

机译:过渡区域一侧加热垂直扁平通道的相对混合对流传热的建模

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In this paper we present results on the numerical investigation of the local opposing mixed convection heat transfer in a vertical flat channel with one-side heating in the laminar and vortex (transitional) regions using FLUENT 6.2 code. The investigations have been performed in airflow of different pressures (0.1, 0.2 and 0.4 MPa) in the range of Re from 1.5·10~3 to 2.5·10~3 and Gr_q from 1.8·10~5 to 2.6·10~7. The cross-section of the test section was 400 mm wide and 40.8 mm high. Channel's heated length was 3890 mm (x/d_e about 50). A hydrodynamic stabilization length of 2370 mm (x/d_e about 25) preceded the heated part of the test section. The value of heat flux on the wall was widely varied in order to achieve different buoyancy effect. Performed numerical modelling with one-side heating demonstrates that under small buoyancy effect, as in the case of symmetrical heating, there are only small transformations in the velocity profile but flow is oriented downwards. With increase of buoyancy forces, the flow separation from the heated wall occurs at some distance from the beginning of the heated channel section. With further increase of buoyancy, the position of flow separation moves towards the beginning of the heated section. Channel wall temperature noticeably decreases at the flow separation point. For the vortex region characteristic sinusoidal flow in the central part of the channel was noticed with the vortices at the heated wall. Correlations for the determination of the position of flow separation from the wall (loss of stability of the flow) in case of one-side heating are suggested. The results of one-side heating have been compared with earlier received results by Poskas et al. [2005] in the vertical flat channel with two-side heating.
机译:在本文中,我们在使用Fluent 6.2码中,在垂直的平面通道中呈现局部相反的混合对流传热的数值调查,使用流利的6.2码。在RE为1.5·10〜3至2.5·10〜3至2.5·10〜3至2.6·10〜7的RE为1.5·10〜3至2.5·10〜3至2.6·10〜7的范围内,在不同压力(0.1,0.2和0.4MPa)的气流中进行了研究。试验部分的横截面为400毫米宽,高40.8毫米。通道的加热长度为3890 mm(x / d_e约50)。水动力稳定长度为2370mm(x / d_e约25)之前的试验部分。为了实现不同的浮力效果,壁上的热量的值被广泛变化。用一侧加热进行的数值建模表明,在小型浮力效应下,如在对称加热的情况下,速度曲线中只有小变换,但流量向下定向。随着浮力力的增加,来自加热壁的流动分离在距离加热通道部分的开始时在一定距离处发生。随着浮力的进一步增加,流动分离的位置朝向加热部分的开头移动。通道壁温在流动分离点处明显减少。对于涡流区域的涡流区域,在频道上的涡流中注意到通道中央部分的正弦流。建议在一个侧加热的情况下,确定与壁的流动分离位置的相关性的相关性。通过POSKAS等人的早期接受结果进行了一侧加热的结果。 [2005]在垂直扁平通道中,具有双侧加热。

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