| Numerical analysis of combustion characteristics of hybrid rocket motor with multi-section swirl injection | |
| Li, Chengen; Cai, Guobiao; Tian, Hui | |
| 刊名 | ACTA ASTRONAUTICA
 |
| 2016 | |
| 卷号 | 123页码:26-36 |
| 关键词 | Hybrid rocket motor Multi-section swirl injection Three-dimensional numerical simulation Combustion flow field Fuel regression rate Combustion efficiency |
| ISSN号 | 0094-5765 |
| DOI | 10.1019/j.actaastro.2016.02.023 |
| URL标识 | 查看原文 |
| 收录类别 | SCIE ; EI |
| WOS记录号 | WOS:000384626700004 |
| 内容类型 | 期刊论文 |
| URI标识 | http://www.corc.org.cn/handle/1471x/5958548 |
| 专题 | 北京航空航天大学 |
| 推荐引用方式 GB/T 7714 | Li, Chengen,Cai, Guobiao,Tian, Hui. Numerical analysis of combustion characteristics of hybrid rocket motor with multi-section swirl injection[J]. ACTA ASTRONAUTICA,2016,123:26-36. |
| APA | Li, Chengen,Cai, Guobiao,&Tian, Hui.(2016).Numerical analysis of combustion characteristics of hybrid rocket motor with multi-section swirl injection.ACTA ASTRONAUTICA,123,26-36. |
| MLA | Li, Chengen,et al."Numerical analysis of combustion characteristics of hybrid rocket motor with multi-section swirl injection".ACTA ASTRONAUTICA 123(2016):26-36. |
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