Effect of Mainstream Velocity on the Optimization of a Fan-Shaped Film-Cooling Hole on a Flat Plate

被引:6
|
作者
Lee, Soo In [1 ]
Jung, Jin Young [1 ]
Song, Yu Jin [1 ]
Kwak, Jae Su [1 ]
机构
[1] Korea Aerosp Univ, Sch Aerosp & Mech Engn, Goyang 10540, South Korea
关键词
fan-shaped hole; film cooling; gas turbine; shape optimization; PERFORMANCE;
D O I
10.3390/en14123573
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
In this study, the effect of mainstream velocity on the optimization of a fan-shaped hole on a flat plate was experimentally investigated. The experiment was conducted by changing the forward expansion angle (beta(fwd)), lateral expansion angle (beta(lat)), and metering length ratio (L-m/D) of the film-cooling hole. A total of 13 cases extracted using the Box-Behnken method were considered to examine the effect of the shape parameters of the film-cooling hole under a 90 m/s mainstream velocity condition, and the results were compared with the results derived under a mainstream velocity of 20 m/s. One density ratio (DR = 2.0) and a blowing ratio (M) ranging from 1.0 to 2.5 were considered, and the pressure-sensitive paint (PSP) technique was applied for the film-cooling effectiveness (FCE). As a result of the experiment, the optimized hole showed a 49.3% improvement in the overall averaged FCE compared to the reference hole with DR = 2.0 and M = 2.0. As the blowing ratio increased, the hole exit area tended to increase, and this tendency was the same as that in the 20 m/s mainstream condition.
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页数:15
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