摘要
The influence of centerline and the cross-section variation to aerodynamic performance of the inlet was researched in a wider range. A new method of measuring the total pressure recovery coefficient and total pressure distortion coefficient of the inlet was proposed. Based on the loitering aircraft, a s-shaped inlet was designed to meet the needs of stable flight of loitering aircraft, whose total pressure recovery coefficient is 93.2% and total pressure distortion coefficient is 1.2%.
| 源语言 | 英语 |
|---|---|
| 主期刊名 | Materials Processing Technology |
| 页 | 349-354 |
| 页数 | 6 |
| DOI | |
| 出版状态 | 已出版 - 2011 |
| 活动 | 2011 International Conference on Advanced Engineering Materials and Technology, AEMT 2011 - Sanya, 中国 期限: 29 7月 2011 → 31 7月 2011 |
出版系列
| 姓名 | Advanced Materials Research |
|---|---|
| 卷 | 291-294 |
| ISSN（印刷版） | 1022-6680 |
会议
| 会议 | 2011 International Conference on Advanced Engineering Materials and Technology, AEMT 2011 |
|---|---|
| 国家/地区 | 中国 |
| 市 | Sanya |
| 时期 | 29/07/11 → 31/07/11 |
指纹
探究 'Design of s-shaped submerged inlet' 的科研主题。它们共同构成独一无二的指纹。引用此
He, G., & Li, X. (2011). Design of s-shaped submerged inlet. 在 Materials Processing Technology (页码 349-354). (Advanced Materials Research; 卷 291-294). https://doi.org/10.4028/www.scientific.net/AMR.291-294.349