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Numerical study of transient conjugate heat transfer of a turbulent impinging jet

机译:湍流射流瞬态共轭传热的数值研究

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This study presents the numerical study of transient conjugate heat transfer in a high turbulence air jet impinging over a flat circular disk. The numerical simulation of transient, two-dimensional cylindrical coordinate, turbulent flow and heat transfer is adopted to test the accuracy of the theoretical model. The turbulent governing equations are resolved by the control-volume based finite-difference method with a power-low scheme, and the well-known low-Re κ-ω turbulence model to describe the turbulent structure. The SIMPLE algorithm is adopted to solve the pressure-velocity coupling. The parameters studied include turbulent flow Reynolds number (Re = 16,100-29,600), heated temperature of a circular disk (T_h = 373 K) or heat flux (q″ = 63-189 kW/m~2), and orifice to heat-source spacing (H/D = 4-10). The numerical results of the transient impinging process indicate that the jet Reynolds number has a significant effect on the hydrodynamics and heat transfer, particularly in the stagnation region of an impinging jet. High turbulence values lead to greater heat transfer coefficients in the stagnation region and cause a bypass of the laminar-to-turbulent transition region in the wall jet region. Induced turbulence from the environment around the jet also influences the variation of the stagnation heat transfer. The modeling approach used here effectively captures both the stagnation region behavior and the transition to turbulence, thus forming the basis of a reliable turbulence model.
机译:这项研究提出了数值研究,在高湍流空气射流撞击平坦的圆盘上瞬态共轭传热。采用瞬态,二维圆柱坐标,湍流和传热的数值模拟来检验理论模型的准确性。湍流控制方程通过基于控制量的有限差分法和低功率方案进行求解,并采用著名的低Reκ-ω湍流模型来描述湍流结构。采用SIMPLE算法求解压力-速度耦合。研究的参数包括湍流雷诺数(Re = 16,100-29,600),圆盘加热温度(T_h = 373 K)或热通量(q''= 63-189 kW / m〜2),以及孔口源间距(H / D = 4-10)。瞬态撞击过程的数值结果表明,射流雷诺数对流体动力学和传热有重要影响,特别是在撞击射流的停滞区域。高湍流值导致在停滞区域中更大的传热系数,并导致壁射流区域中的层流到湍流过渡区域的旁路。射流周围环境引起的湍流也影响停滞传热的变化。这里使用的建模方法有效地捕获了停滞区域的行为和向湍流的过渡,从而形成了可靠的湍流模型的基础。

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