期刊文献+
共找到1篇文章
< 1 >
每页显示 20 50 100
Effect of cross-flow direction of coolant on film cooling effectiveness with one inlet and double outlet hole injection 被引量:2
1
作者 guangchao lin Chaolin Wu +2 位作者 Wei Zhang Zhihai Kou Dawei Peng 《Propulsion and Power Research》 SCIE 2012年第1期71-77,共7页
In order to study the effect of cross-flow directions of an internal coolant on film cooling performance,the discharge coefficients and film cooling effectiveness with one inlet and double outlet hole injections were ... In order to study the effect of cross-flow directions of an internal coolant on film cooling performance,the discharge coefficients and film cooling effectiveness with one inlet and double outlet hole injections were simulated.The numerical results show that two different cross-flow directions of the coolant cause the same decrease in the discharge coefficients as that in the case of supplying coolant by a plenum.The different proportion of the mass flow out of the two outlets of the film hole results in different values of the film cooling effectiveness for three different cases of coolant supplies.The film cooling effectiveness is the highest for the case of supplying coolant by the plenum.At a lower blowing ratio of 1.0,the film cooling effectiveness with coolant injection from the right entrance of the passage is higher than that from the left entrance of the passage.At a higher blowing ratio of 2.0,the opposite result is found. 展开更多
关键词 Aerospace propulsion system Turbine blade Film cooling CROSS-FLOW Numerical simulation
原文传递
上一页 1 下一页 到第
使用帮助 返回顶部