| Coupled heat transfer analysis of thrust chambers with recessed shear coaxial injectors | |
| Song, Jiawen; Sun, Bing | |
| 刊名 | ACTA ASTRONAUTICA
 |
| 2017 | |
| 卷号 | 132页码:150-160 |
| 关键词 | Liquid rocket engine Turbulent combustion Regenerative cooling Thrust chamber Injector recess Heat transfer |
| ISSN号 | 0094-5765 |
| DOI | 10.1016/j.actaastro.2016.12.026 |
| URL标识 | 查看原文 |
| 收录类别 | SCIE ; EI |
| WOS记录号 | WOS:000394636100019 |
| 内容类型 | 期刊论文 |
| URI标识 | http://www.corc.org.cn/handle/1471x/5941803 |
| 专题 | 北京航空航天大学 |
| 推荐引用方式 GB/T 7714 | Song, Jiawen,Sun, Bing. Coupled heat transfer analysis of thrust chambers with recessed shear coaxial injectors[J]. ACTA ASTRONAUTICA,2017,132:150-160. |
| APA | Song, Jiawen,&Sun, Bing.(2017).Coupled heat transfer analysis of thrust chambers with recessed shear coaxial injectors.ACTA ASTRONAUTICA,132,150-160. |
| MLA | Song, Jiawen,et al."Coupled heat transfer analysis of thrust chambers with recessed shear coaxial injectors".ACTA ASTRONAUTICA 132(2017):150-160. |
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