低雷诺数下横流增强射流冲击换热

G. Failla, E. H. Bishop, J. Liburdy
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引用次数: 9

摘要

通过实验研究了独立控制横流的圆形射流对翅片表面的传热和流动特性的影响。射流阵列被配置为撞击矩形鳍的顶部,而横流被引导通过由鳍形成的通道。对几种不同几何形状的机翼进行了试验,以确定在仅射流撞击、仅横流和射流与横流相结合的情况下的总体换热情况。结果以驱动流动所需的压力以及射流和通道雷诺数的形式呈现。努塞尔数相关性表明,能够优化射流和横向流动与鳍的几何形状,以获得特定的传热条件。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
ENHANCED JET IMPINGEMENT HEAT TRANSFER WITH CROSSFLOW AT LOW REYNOLDS NUMBERS
An experimental investigation was conducted to determine the heat transfer and flow characteristics for a finned surface subject to circular impinging jets with independently controlled crossflow. The jet array was configured to impinge on the top of the rectangular fins while the crossflow was directed through the channels formed by the fins. Tests were performed to determine the overall heat transfer under conditions of only jet impingement, only crossflow and combined jet with crossflow, for several fin geometries. Results are presented in terms of necessary pressure to drive the flow as well as in terms of the jet and channel Reynolds numbers. Nusselt number correlations indicated the ability to optimize the jet and crossflow with the fin geometry to obtain specific heat transfer conditions.
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