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FLOW AND HEAT TRANSFER OF AIR ROUND JET FLOWING INSIDE A HOT CYLINDRICAL CAVITY

机译:空气圆射流流动在热圆柱腔内流动和传热

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The flow structure and heat transfer characteristics of a turbulent axisymmetric jet flowing into a heated cylindrical cavity. It comes to a jet exiting into a cavity with a closed bottom, open to the ambient air upstream. This flow configuration is encountered in several industrial applications such as the cooling system or the ventilation of confined spaces. This problem parameters are: (a) jet exit Reynolds number (Re, based on the nozzle diameter; d) ranged from 20000 to 50000, (b); the non-dimensional distance from the jet exit and the cavity bottom (Lf) between 2 and 8. The Reynolds Stress second order turbulence model coupled to the enhanced wall treatment is used for the numerical predictions. The flow structure interaction between the jet exit and the cavity bottom area is detailed through the velocity profiles. The thermal study was based on the influence of the Reynolds number Re and the impinging distance Lf on the local Nusselt number. The computations agree well with available data. Numerical results show that, both flow and heat transfer was significantly affected by impinging distance and Reynolds number. The distribution of average Nusselt number is correlated according with some problem parameters (Nuavr=f(Re, Lf)).
机译:湍流轴对称射流的流动结构和热传递特性流入加热的圆筒形腔。它涉及到离开进入具有封闭底部,开放至环境空气上游的腔的喷射。这种流动配置在若干工业应用中遇到,如冷却系统或有限空间的通风。此问题的参数是:(a)喷射出口雷诺数(Re,基于喷嘴的直径; d)介于20000至50000;(B);从喷射出口和所述非三维距离2和8之间的空腔底部(LF),其耦合至增强壁治疗雷诺应力二阶湍流模型被用于数值预测。喷射出口和腔体底部区域之间的流动结构交互是通过速度分布详述。热研究的基础上,雷诺数Re和对当地Nu数撞击距离Lf的影响。该计算与现有数据吻合。计算结果表明,无论是流动和传热进行显著受撞击的距离和雷诺数。平均努塞尔数的分布的一些问题的参数(Nuavr = F(RE,LF))根据相关。

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