Knowledge Resource Center for Ecological Environment in Arid Area
| 报告编号 | NACA-TM-1150 |
| 来源ID | NTRS_Document_ID: 20050019417 |
| Compression Shocks of Detached Flow | |
| Eggink | |
| 英文摘要 | It is known that compression shocks which lead from supersonic to subsonic velocity cause the flow to separate on impact on a rigid wall. Such shocks appear at bodies with circular symmetry or wing profiles on locally exceeding sonic velocity, and in Laval nozzles with too high a back pressure. The form of the compression shocks observed therein is investigated. |
| 英文关键词 | SHOCK WAVES SEPARATED FLOW WALL FLOW FLOW DISTRIBUTION |
| 出版年 | 1947 |
| 报告类型 | Technical Report |
| 语种 | 英语 |
| 国家 | 美国 |
| URL | http://hdl.handle.net/2060/20050019417 |
| 资源类型 | 科技报告 |
| 条目标识符 | http://119.78.100.177/qdio/handle/2XILL650/258343 |
| 推荐引用方式 GB/T 7714 | Eggink. Compression Shocks of Detached Flow,1947. |
| 条目包含的文件 | 条目无相关文件。 | |||||
| 个性服务 |
| 推荐该条目 |
| 保存到收藏夹 |
| 导出为Endnote文件 |
| 谷歌学术 |
| 谷歌学术中相似的文章 |
| [Eggink]的文章 |
| 百度学术 |
| 百度学术中相似的文章 |
| [Eggink]的文章 |
| 必应学术 |
| 必应学术中相似的文章 |
| [Eggink]的文章 |
| 相关权益政策 |
| 暂无数据 |
| 收藏/分享 |
除非特别说明，本系统中所有内容都受版权保护，并保留所有权利。
