Supersonic - Subsonic Transition in Relatively Narrow Channels
文献类型：期刊论文
| 作者 | Rudolf Dvorak |
| 刊名 | JOURNAL OF THERMAL SCIENCE
 |
| 出版日期 | 2000 |
| 卷号 | 9期号:4页码:311，315 |
| 关键词 | Internal Aerodynamics Compressible Flow Channel Flow Shock Waves |
| 英文摘要 | The flow structure in relatively narrow channels has a strong three-dimensional character with complex flow phenomena, including regions of localized separation, various vortical structures, etc., all of which have to be considered when dealing with the problem of supersonic-subsonic transition. In this paper only the following three problems are considered: 1. the effect of channel width on transition from supersonic to subsonic velocities, 2. transition from supersonic to subsonic velocities in a system of shock waves - pseudoshock wave, 3. transition from subsonic to supersonic velocities in a critical cross section at the end of a duct with fully developed turbulent channel flow. Problems connected with vortical structures and flow separation were discussed by the same author elsewhere (see References). |
| 公开日期 | 2013-03-12 |
| 源URL | [http://ir.etp.ac.cn/handle/311046/53852]  |
| 专题 | 工程热物理研究所_Journal of Thermal Science |
| 推荐引用方式 GB/T 7714 | Rudolf Dvorak. Supersonic - Subsonic Transition in Relatively Narrow Channels[J]. JOURNAL OF THERMAL SCIENCE,2000,9(4):311，315. |
| APA | Rudolf Dvorak.(2000).Supersonic - Subsonic Transition in Relatively Narrow Channels.JOURNAL OF THERMAL SCIENCE,9(4),311，315. |
| MLA | Rudolf Dvorak."Supersonic - Subsonic Transition in Relatively Narrow Channels".JOURNAL OF THERMAL SCIENCE 9.4(2000):311，315. |
入库方式： OAI收割
来源：工程热物理研究所
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