Numerical Approach to Film Cooling Effectiveness Over a Plate Surface with Coolant Impingement
文献类型：期刊论文
| 作者 | Chang-Hsien Tail; Jr-Ming Miao2; A-Fu Kao3 |
| 刊名 | JOURNAL OF THERMAL SCIENCE
 |
| 出版日期 | 2004 |
| 卷号 | 13期号:1页码:67,74 |
| 关键词 | Film Cooling Impingement Cooling Cfd Turbulence Model. |
| 英文摘要 | The aim of the present study is conducting the numerical approach to a combination of internal jet impingement and external film cooling over a flat plate. A multi-block three-dimensional Navier-Stokes code, CFX 4.4, with k-ε turbulence model is used to simulate this complicated thermal-flow structure induced by the interaction of coolant jet and hot cross mainstream. By assuming the adiabatic wall boundary condition on the tested film-cooled plate, both the local and the spanwise-averaged adiabatic film cooling effectiveness are evaluated for comparison of the cooling performance at blowing ratios of Br=0.5, 1.0, and 1.5. Film flow data were obtained from a row of five cylindrical film cooling holes, inclined in angle of 35° and 0° in direction of streamwise and spanwise, respectively. The film cooling hole spacing between adjacent holes is 15 mm for all the holes. Before the coolant flow being injected through individual cooling hole then encountered with the mainstream, an impingement chamber containing an impingement plate with 43 holes is located on the path of coolant flow. Present study also focused on the effect of impingement spacing, 10mm, 20mm, and 30mm. Compare the results, we find the impingement jet has a significant effect on the adiabatic film cooling effectiveness. As the coolant impingement spacing is fixed, results indicated that higher blowing ratio would enhance the local and the spanwise-averaged adiabatic film cooling effectiveness. Moreover, neither uniform nor parabolic distribution of pressure distribution are observed within the coolant hole-pipe. |
| 公开日期 | 2013-03-11 |
| 源URL | [http://ir.etp.ac.cn/handle/311046/53294]  |
| 专题 | 工程热物理研究所_Journal of Thermal Science |
| 推荐引用方式 GB/T 7714 | Chang-Hsien Tail,Jr-Ming Miao2,A-Fu Kao3. Numerical Approach to Film Cooling Effectiveness Over a Plate Surface with Coolant Impingement[J]. JOURNAL OF THERMAL SCIENCE,2004,13(1):67,74. |
| APA | Chang-Hsien Tail,Jr-Ming Miao2,&A-Fu Kao3.(2004).Numerical Approach to Film Cooling Effectiveness Over a Plate Surface with Coolant Impingement.JOURNAL OF THERMAL SCIENCE,13(1),67,74. |
| MLA | Chang-Hsien Tail,et al."Numerical Approach to Film Cooling Effectiveness Over a Plate Surface with Coolant Impingement".JOURNAL OF THERMAL SCIENCE 13.1(2004):67,74. |
入库方式： OAI收割
来源：工程热物理研究所
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