Transonic Instability in Entrance Part of Mixing Chamber of High-Speed Ejector
文献类型：期刊论文
| 作者 | Vaclav Dvorak1; Pavel Safarik2 |
| 刊名 | JOURNAL OF THERMAL SCIENCE
 |
| 出版日期 | 2005 |
| 卷号 | 14期号:3页码:258,263 |
| 关键词 | Transonic Instability Ejector Shock Waves |
| 英文摘要 | The paper deals with experimental and numerical study of flow structure in two-dimensional model of supersonic ejector. Schlieren pictures of flow structure were taken, static pressure distributions on side wall were measured and Fluent software to calculate the flow structure in supersonic ejector was used. For certain region of back pressure ratio pb/p02 and stagnation pressure ratio of both streams p01/p02 the terminal shock wave is close to the trailing edge of the primary flow nozzle and a transonic instability occurs. The instability causes the movement of position of boundary layer separation, the structure of shock waves changes and all flow structure oscillates. The movie of these regimes during schlieren experiments was taken and relevant numerical modelling was performed. |
| 公开日期 | 2013-03-11 |
| 源URL | [http://ir.etp.ac.cn/handle/311046/53232]  |
| 专题 | 工程热物理研究所_Journal of Thermal Science |
| 推荐引用方式 GB/T 7714 | Vaclav Dvorak1,Pavel Safarik2. Transonic Instability in Entrance Part of Mixing Chamber of High-Speed Ejector[J]. JOURNAL OF THERMAL SCIENCE,2005,14(3):258,263. |
| APA | Vaclav Dvorak1,&Pavel Safarik2.(2005).Transonic Instability in Entrance Part of Mixing Chamber of High-Speed Ejector.JOURNAL OF THERMAL SCIENCE,14(3),258,263. |
| MLA | Vaclav Dvorak1,et al."Transonic Instability in Entrance Part of Mixing Chamber of High-Speed Ejector".JOURNAL OF THERMAL SCIENCE 14.3(2005):258,263. |
入库方式： OAI收割
来源：工程热物理研究所
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