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Heat transfer characteristics of gaseous slip flow in a micro-channel

机译:微通道中气体滑流的传热特性

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Two-dimensional compressible momentum and energy equations with slip boundary conditions are solved to obtain the heat transfer characteristics of gaseous slip flow in a micro-channel with CWT (constant wall temperature) whose temperature is lower or higher than the inlet temperature (cooled case or heated case). The numerical methodology is based on the Arbitrary-Lagrangian-Eulerian (ALE) method. The stagnation temperature is fixed at 300 K and the computations were done for the wall temperature which ranges from 250 K to 350 K. The channel height ranges from 2 to 10 μm and the channel aspect ratio is 200. The stagnation pressure is chosen in such a way that the exit Mach number ranges from 0.1 to 0.7. The outlet pressure is fixed at atmospheric condition. The bulk temperature and the total temperature of the heated case are compared with those of the cooled case and also compared with temperatures of the incompressible flow in a conventional sized channel. Heat transfer characteristics of the gaseous flow are different from those of the liquid flow. And they are also different from each cooled and heated case. A correlation for the prediction of the heat transfer rate of the gaseous slip flow in a micro-channel is proposed.
机译:求解具有滑移边界条件的二维可压缩动量和能量方程,以获得CWT(恒定壁温)温度低于或高于入口温度(冷却箱或冷却箱)的微通道中气态滑流的传热特性。加热箱)。数值方法基于任意拉格朗日欧拉(ALE)方法。停滞温度固定为300 K,计算壁温范围为250 K至350K。通道高度为2至10μm,通道纵横比为200。在这种情况下选择停滞压力出口马赫数在0.1到0.7之间的一种方式。出口压力固定在大气压下。将加热壳体的整体温度和总温度与冷却壳体的整体温度和总温度进行比较,并且还与常规尺寸通道中不可压缩流的温度进行比较。气流的传热特性不同于液体的传热特性。而且它们也与每个冷却和加热的情况不同。提出了一种用于预测微通道中气态滑流的传热速率的相关性。

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