Influence of orientation angles of branch hole on film cooling effectiveness with one inlet and double outlet hole injection
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Influence of orientation angles of branch hole on film cooling effectiveness with one inlet and double outlet hole injection
Vol. 26, Issue 7, (2011)
作者机构:
沈阳航空航天大学 动力与能源工程学院 辽宁省数字化工艺仿真与试验技术重点实验室,沈阳,110136
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Published:2011
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LI Guang-chao, WU Dong, ZHANG Wei, et al. Influence of orientation angles of branch hole on film cooling effectiveness with one inlet and double outlet hole injection[J]. 2011, 26(7).
DOI:
LI Guang-chao, WU Dong, ZHANG Wei, et al. Influence of orientation angles of branch hole on film cooling effectiveness with one inlet and double outlet hole injection[J]. 2011, 26(7).DOI:
Influence of orientation angles of branch hole on film cooling effectiveness with one inlet and double outlet hole injection
In order to investigate the influence of orientation angles of branch hole on film cooling effectiveness with one inlet and double outlet hole injection
the film cooling effectiveness was simulated by commercial code using the finite volume method
on the condition that the orientation angles of branch hole were 30°
45°
60° and 90° respectively
the blowing ratios varied from 0.5 to 2.0 . The flow field
the film cooling effectiveness and the spanwise averaged film cooling effectiveness were investigated. The results show that the film cooling effectiveness with one inlet and double outlet hole injection has been improved as compared to that of the cylindrical hole injection. The optimized branch hole angle is 45°
higher by 300% than the film cooling effectiveness of the cylindrical hole injection. The orientation angles of branch hole have an increasing influence on the film cooling effectiveness with the increase of blowing ratios.
Effect of rotation on the leading-edge region film cooling of a twisted turbine blade
Effect of the shape of divider wall on heat transfer and flow resistance characteristic of passage
Numerical simulation of film cooling effectiveness with one inlet and double outlet hole on leading edge
Influence of rotation on discharge coefficients of two rows of film holes in channel with rib turbulators
Numerical simulation of cooling effectiveness with injection of double-outlet hole
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