| Citation: | DENG Ming-chun, ZHU Hui-ren, WANG Xue-wen, XU Du-chun. Influence of density ratio on the discharge coefficient of turbine blade film cooling holes[J]. Journal of Aerospace Power, 2006, 21(5): 795-799. |
| [1] |
Hay N,Lampard D,Benmansour S.Effects of crossflows on the discharge coefficient of film cooling holes[J].ASME Journal of Engineering for Power,1983,105:243-374.
|
| [2] |
Hay N,Henshall S E,Manning A.Discharge coefficient of holes angled to the flow direction[J].ASME Journal of Turbomachinery,1994,116:358-368.
|
| [3] |
Hay N,Spencer A.Discharge coefficient of film cooling holes with radiused and chamfered inlets[R].ASME Paper No.91-GT-269,1991.
|
| [4] |
Petersen D R,Eckert E R G,Goldstein R J.Filming cooling with large density differences between the mainstream and secondary fluid measured by heat-mass transfer analogy[J].ASME Journal of Heat Transfer,1997,99:620-627.
|
| [5] |
朱惠人,许都纯,刘松龄.气膜孔形状对流量系数影响的实验研究[J].推进技术,1998,19(1):42-45.Zhu Huiren,Xu Duchun,Liu Songling.The experimental investigation in the effects of film cooling holes shape on discharge coefficient[J].Journal of Propulsion Technology,1998,19 (1):42-45.
|
| [6] |
向安定,朱惠人,刘松龄,等.涡轮导向叶片表面气膜孔流量系数的实验研究[J].推进技术,2003,24(3):216-218.Xiang Anding,Zhu Huiren,Liu Songling,et al.Discharge coefficient measurements for film cooling holes on blade surface in a turbine cascade[J].Journal of Propulsion Technology,2003,24(3):216-218.
|
| [7] |
许都纯,刘松龄,游绍堃,等.低速大尺寸传热风洞的研制[J].推进技术,1997,18(2):61-64.Xu Duchun,Liu Songling,You Shaokun,et al.Setting-up and investigation of a large-scale low-speed heat-transfer wind tunnel[J].Journal of Propulsion Technology,1997,18(2):61-64.
|