FILM COOLING FROM SHORT HOLES WITH SISTER HOLE INFLUENCE

被引:0
|
作者
Ely, Marc J. [1 ]
Jubran, B. A. [1 ]
机构
[1] Ryerson Univ, Dept Aerosp Engn, Aerothermal Management Lab, Toronto, ON M5B 2K3, Canada
关键词
IN-CROSS-FLOW; JET;
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper reports a computational analysis on the effect of sister hole control on film cooling from short holes. The proposed method includes surrounding a primary injection hole by two or four smaller sister holes to actively maintain flow adhesion along the surface of the blade. A numerical study using the realizable k-epsilon turbulence model led to the determination that the use of sister holes significantly improves adiabatic effectiveness by countering the primary vortical flow structure. Research was carried out to determine the optimum hole configuration, arriving at the conclusion that placing sister holes slightly downstream of the primary injection hole improves the near-hole effectiveness, while placing sister holes slightly upstream of the primary hole improves downstream effectiveness. Similar results were found in evaluating both long and short hole geometries with a significantly less coherent flow field arising from the short hole. However, on the whole, the sister hole approach to film cooling was found to offer viable improvements over standard cooling regimes.
引用
收藏
页码:1185 / 1196
页数:12
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