Conjugate heat transfer analysis on double-wall cooling configuration including jets impingement and film holes with conformal pins

Chenlin Chen, Yuting Jiang, Haosu Zhang, Liangchen Dong, Zitong Zhang
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Abstract

A double-wall cooling configuration including impingement holes and film holes with conformal pins is studied by CFD numerical simulation in this paper. The influences of three different injection directions of film holes at six blowing ratios ranging from 0.4 to 2.5 on conjugate heat transfer characteristic are investigated. Impingement-only arrangements with corresponding pin directions are adopted to illustrate the film cooling gains and the impingement cooling contribution. The results indicate that the effect of different pin directions on overall cooling effectiveness is non-significant. At low blowing ratio, the forward injection arrangement has higher overall cooling effectiveness since greater gain of film cooling, and is transcended by reverse injection arrangement as coolant supplement increases. Moreover, although the cooling effectiveness for normal injection case is the lowest within the whole range of mass flow rate, it possesses the most uniform distribution of cooling effectiveness in downstream region at high blowing ratio.
双壁冷却配置的共轭传热分析,包括喷流撞击和带保形销的膜孔
本文通过 CFD 数值模拟研究了一种双壁冷却结构,包括带保形销的撞击孔和薄膜孔。研究了在 0.4 至 2.5 的六个吹气比范围内,薄膜孔的三种不同喷射方向对共轭传热特性的影响。采用了相应针孔方向的纯撞击布置来说明薄膜冷却增益和撞击冷却贡献。结果表明,不同针方向对整体冷却效果的影响并不显著。在低吹气比情况下,正向喷射布置由于薄膜冷却增益更大而具有更高的整体冷却效果,而随着冷却剂补充量的增加,反向喷射布置的冷却效果将被超越。此外,虽然在整个质量流量范围内,正向喷射的冷却效果最低,但在高吹气比时,它在下游区域的冷却效果分布最均匀。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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