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CONVECTIVE HEAT TRANSFER OF UNCHOKED AND CHOKED GAS FLOW IN MICRO-TUBES

机译:微管中未混沌和窒息气流的对流传热

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Heat transfer characteristics of unchoked and choked gas flows in micro-tubes with constant wall temperature were numerically investigated both laminar and turbulent flow cases. The numerical methodology is based on the Arbitrary-Lagrangian-Eulerian (ALE) method. The Lam-Bremhorst Low-Reynolds number turbulence model was used for turbulent flow. The compressible momentum and energy equations with the assumption of the ideal gas were solved. The computational domain should be extended to the downstream region of the hemisphere from micro-tube outlet. The back pressure was given to the outside of the downstream region. The stagnation temperature is fixed at 300K and the computations were done for the wall temperature which ranges from 305K to 350K. The tube diameter ranges from 50 to 250 |im and tube aspect ratio is 200. The stagnation pressure is chosen in such a way that the flow at micro-tube exit is enough to be fully under-expanded. By increasing the stagnation pressure, the internal flow in the micro-tube is choked and the flow at the micro-tube outlet is under-expanded. Although the velocity remains constant, the mass flow rate (Reynolds number) increases. The results in a wide range of Reynolds number and Mach number were obtained. The bulk temperature based on the static temperature and the total temperature are compared with those of the incompressible flow. A correlation for the prediction of the heat transfer rate of the unchoked and choked gas flow in micro-tubes is proposed.
机译:在具有恒定壁温的微管中,在具有恒定壁温的微管中流动的传热特性在数值上进行了数值研究了层流和湍流流箱。数值方法基于任意拉格朗日 - 欧拉(ALE)方法。 LAM-BREMHORST低雷诺数湍流模型用于湍流。解决了具有假设理想气体的可压缩动力和能量方程。计算域应延伸到从微管出口的半球的下游区域。向后压力给下游区域的外部。停滞温度固定在300k,并为壁温进行计算,其范围为305k至350k。管直径范围为50至250 | IM和管宽比为200.以这样的方式选择停滞压力,使得微管射出的流动足以完全膨胀。通过增加停滞压力,窒息微管中的内部流动,并且膨胀微管出口处的流动。虽然速度保持恒定,但质量流量(雷诺数)增加。获得了各种雷诺数和马赫数的结果。将基于静态温度和总温度的体积温度与不可压缩的流动进行比较。提出了对微管中未记录和窒息气流的传热速率预测的相关性。

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