A Numerical Study on the 2D Film Cooling of a Flat Surface

被引:22
作者
Singh, Kuldeep [1 ]
Premachandran, B. [1 ]
Ravi, M. R. [1 ]
机构
[1] Indian Inst Technol Delhi, Dept Mech Engn, New Delhi 110016, India
关键词
CROSS-FLOW; STREAMWISE ANGLES; HEAT-TRANSFER; FOREIGN GAS; PART I; INJECTION; DENSITY; TURBULENCE; HOLES; JET;
D O I
10.1080/10407782.2014.949131
中图分类号
O414.1 [热力学];
学科分类号
摘要
In this article, the results obtained from a detailed numerical investigation of 2D film cooling over a flat plate through single-slot injection are presented. The effects of mainstream Reynolds number, blowing ratio, density ratio, and injection angle on the effectiveness of film cooling were investigated in the present work. Numerical simulations were carried over a wide range of density ratio ranging from 1.1 to 5 at two mainstream Reynolds numbers (8x10(4) and 1.5x10(5)), three blowing ratios (ranging from 1 to 3), and six injection angles (ranging from 15 degrees to 90 degrees). The results show that at lower injection angles of 15 degrees-45 degrees, maximum film-cooling effectiveness occurs at a particular value of velocity ratio which is found to be independent of mainstream Reynolds number, blowing ratio, and density ratio. Based on a combined effect analysis of blowing ratio, density ratio, and injection angle, a relation was obtained for velocity ratio that gives an optimum film-cooling effectiveness.
引用
收藏
页码:673 / 695
页数:23
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