Heat transfer in a rotating two-inlet wedge-shaped channel with pin-fins

•A two-inlet pin-fin arrayed wedge-shaped channel is experimentally studied.•A comprehensive comparison of data with related literatures are conducted.•Rotational effects on heat transfer can be suppressed in two-inlet channel.•Effects of channel orientation is different for radial inward or outward...

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Bibliographic Details
Published inInternational journal of heat and mass transfer Vol. 163; p. 120380
Main Authors Li, Hua, Deng, Hongwu, Bai, Lei, Zhu, Jianqin, Tian, Shuqing, Qiu, Lu
Format Journal Article
LanguageEnglish
Published Oxford Elsevier Ltd 01.12.2020
Elsevier BV
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Summary:•A two-inlet pin-fin arrayed wedge-shaped channel is experimentally studied.•A comprehensive comparison of data with related literatures are conducted.•Rotational effects on heat transfer can be suppressed in two-inlet channel.•Effects of channel orientation is different for radial inward or outward flow. Heat transfer in rotating channels attracts a significant amount of research attentions due to its application in turbomachinery. The current work focuses on the heat transfer in a pin-fin-arrayed wedge-shaped channel with multiple inlets and outlets, which is a typical model of the internal cooling passage in a turbine blade trailing tail. Unlike the traditional single-inlet channel, the two-inlet configuration generates a counteractive flow which could improve the heat transfer uniformity in the channel. The overall Reynolds number and rotation number that are evaluated with the total mass-flowrate vary from 20,000 to 45,000 and 0 to 0.155, respectively. In rotating conditions, a critical mass-flowrate ratio can be identified, where the rotational effect can be neglected, suggesting that the rotational effects on heat transfer could be suppressed by introducing the second stream of coolant. Finally, the data in the current work are compared with the previous measurements conducted in the channels with different channel orientation, turbulator and channel cross-section. It is found that the rotational effect is sensitive to channel orientation regardless of cross-section and turbulators.
ISSN:0017-9310
1879-2189
DOI:10.1016/j.ijheatmasstransfer.2020.120380