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Investigation of natural convection heat transfer to the cooled top boundary of a heated pool

机译:自然对流传热到加热池冷却顶部边界的研究

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Experiments have been performed in the framework of the BALl program for the investigation of turbulent heat transport to the upper cooled top boundary of a volumetrically heated pool. A specific LIF (laser induced fluorescence) technique has been used to visualise the plumes detaching from the top boundary. Results concerning flow configurations, detachment time intervals. size of plumes and characteristic distances between plumes will be presented as a function of Rayleigh and Prandtl numbers. A model has been developed for the description of these plumes and the resulting heat transfer. A physical understanding of the effect of Rayleigh and Prandtl numbers on heat transfer has been gained. The so-called soft turbulence regime is associated with negligible interaction between plumes detaching from the boundary and the main flow. In this regime, the Nusselt number is proportional to Ra~(1/3). The so-called hard turbulence regime is associated with an interaction between the plumes and the main flow. The plumes are locally and intermittently destroyed by a laminar boundary layer developing from large eddies issued from the main flow and impacting the boundary. The development of these laminar layers explains the dependency of the Nusselt number as approximately Ra~(2/7) in this regime. For elevated Rayleigh numbers, the increase of the Reynolds number in the main flow explains the development of fully turbulent boundary layers. In the so-called asymptotic regime, experiments by Chavanne (1997) have shown that Nusselt is approximately proportional to Ra~0.4. Effects of the aspect ratio have been reported.
机译:已经在BAL1程序的框架内进行了实验,以研究湍流热传递到容积加热池的上部冷却顶部边界。特定的LIF(激光诱导荧光)技术已用于可视化从顶部边界脱离的羽流。有关流量配置,拆卸时间间隔的结果。羽的大小和羽之间的特征距离将作为瑞利和普朗特数的函数给出。已经开发了用于描述这些羽流和由此产生的热传递的模型。已经获得了对瑞利和普朗特数对传热影响的物理理解。所谓的软湍流状态与从边界脱离的羽流和主流之间的相互作用可忽略不计。在这种情况下,Nusselt数与Ra〜(1/3)成正比。所谓的强湍流状态与羽流和主流之间的相互作用有关。羽流被层状边界层局部断断续续破坏,该边界层是由主流产生的大涡流形成的,并冲击边界。这些层状层的发展解释了在该状态下努塞尔特数的依赖性约为Ra〜(2/7)。对于升高的瑞利数,主流中雷诺数的增加解释了完全湍流边界层的发展。在所谓的渐近状态下,Chavanne(1997)的实验表明,Nusselt近似与Ra〜0.4成正比。已经报道了纵横比的影响。

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