Abstract

Regarding the cooling structure of gas turbine combustors, this paper employs numerical simulation methods to analyze the influence of structural parameters of a rectangular trench with inclined holes on flow and heat transfer characteristics at a coolant-side Reynolds number of 100,000. The results indicate that with a decrease in the width of the rectangular trench and an increase in the diameter of the inclined holes, the coolant-side friction factor gradually decreases. The coolant-side friction factor at a streamwise distance of Y/D = 30 is lower than that at Y/D = 20 and 40. With an increase in the diameter of the inclined holes, the average coolant-side Nusselt number exhibits a greater increase, indicating significantly enhanced heat transfer effectiveness. The average coolant-side Nusselt number at a streamwise distance of Y/D = 40 is higher than that at Y/D = 20 and 30. Furthermore, with an increase in the diameter of the inclined holes and a decrease in the streamwise distance, the average temperature of the solid wall on the hot-gas side gradually decreases, leading to a progressive improvement in cooling efficiency.

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Year
2025
Type
article
Volume
18
Issue
24
Pages
6441-6441
Citations
0
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Liang Xu, Yi Wan, Lei Xi et al. (2025). Effects of Rectangular Trench and Inclined Hole Geometry on Film Cooling Flow and Heat Transfer Characteristics. Energies , 18 (24) , 6441-6441. https://doi.org/10.3390/en18246441

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DOI
10.3390/en18246441