西安交通大学能源与动力工程学院,西安,710049
网络首发:2014-03-10,
纸质出版:2014
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廖高良, 王新军, 李军. 带槽双射流气膜冷却数值研究[J]. 西安交通大学学报, 2014,48(3):34-38+127.
Numerical Investigation to Double-Jet Film-Cooling with Trench[J]. 2014, 48(3): 34-38+127.
廖高良, 王新军, 李军. 带槽双射流气膜冷却数值研究[J]. 西安交通大学学报, 2014,48(3):34-38+127. DOI: 10.7652/xjtuxb201403007.
Numerical Investigation to Double-Jet Film-Cooling with Trench[J]. 2014, 48(3): 34-38+127. DOI: 10.7652/xjtuxb201403007.
针对双射流气膜冷却在提高气膜冷却效率中存在横向冷却效果不佳的问题
提出了一种带槽结构的双射流气膜冷却方式
即在气膜孔出口处垂直于流向横开一槽
并在平均吹风比为1.9时
采用CFX商用软件及剪切应力输运湍流模型对带槽双射流结构的流动与冷却特性进行数值研究
获得了横槽倾角对气膜冷却特性的影响规律。研究结果表明:在相同孔间距下
带槽结构能明显改善气膜在被冷却壁面的横向分布
增大气膜的横向覆盖面积
有效提高气膜冷却效率; 不同的横槽倾角对气膜冷却效率具有重要的影响
倾角均为30°时的方案冷却效果最好; 沿中心线远离气膜孔处出现未冷却区域
这可能与吹风比、横槽倾角、槽宽等参数有关。研究结果为射流冷却的流动与换热特性研究提供了参考依据。
Double-jet film-cooling is able to significantly improve the film cooling effect
whereas has poor lateral cooling result. A new double-jet film cooling with trench is presented. The film holes are embedded in transverse trench perpendicular to the flow direction. To consider the influence of trench inclined angles on the film cooling characteristic
commercial software CFX and shear stress transport(SST)turbulence model are applied to numerically investigate the flow and film cooling characteristics of the double-jet film-cooling with trench at the averaged blowing ratio of 1.9. It is shown that the configuration with trench obviously improves the film transverse distribution on the cooled surfaces
and increases the film transverse cover area and enhances the film cooling effectiveness. The trench inclined angle greatly affects film cooling effectiveness
which reaches the best in the case of 30°. An uncooled zone far from the film holes along the centerline is found
which may be related to the blowing ratio
trench inclined angles and trench width.
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刘存良, 朱惠人, 白江涛. 收缩-扩张形气膜孔提高气膜冷却效率的机理研究[J]. 航空动力学报, 2008, 23(4): 992-996.
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KUSTERER K, BOHN D, SUGIMOTO T. Double-jet ejection of cooling air for improved film cooling[J]. ASME Journal of Turbomachinery, 2007, 129(10): 809-815.
KUSTERER K, BOHN D, SUGIMOTO T. Influence of blowing ratio on the double-jet ejection of cooling air[C]∥Proceedings of ASME Turbo Expo 2007. New York, USA: ASME, 2007: 305-315.
KUSTERER K, ELYAS A, BOHN D. Double-jet film- cooling for highly efficient film-cooling with low blowing ratios[C]∥Proceedings of ASME Turbo Expo 2008. New York, USA: ASME, 2008: 23-34.
KUSTERER K, ELYAS A, BOHN D. A parametric study on the influence of the lateral ejection angle of double-jet holes on the film cooling effectiveness for high blowing ratios[C]∥Proceedings of ASME Turbo Expo 2009. New York, USA: ASME, 2009: 199-211.
KUSTERER K, ELYAS A, BOHN D. Film cooling effectiveness comparison between shaped-and double-jet film cooling holes in a row arrangement[C]∥Proceedings of ASME Turbo Expo 2010. New York, USA: ASME, 2010: 1503-1515.
LU Y P, DHUNGEL A, EKKAD S V. Effect of trench width and depth on film cooling from cylindrical holes embedded in trenches[C]∥Proceedings of ASME Turbo Expo 2007. New York, USA: ASME, 2007: 28-39.
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