摘要
Rocket engine thrust is the main performance parameters. The flow field of missile fight in different Mach is simulated by using FLUENT, then calculating the thrust of different conditions. The calculating results are consistent with the theory of Mach almost no effect on the thrust.
| 源语言 | 英语 |
|---|---|
| 主期刊名 | Materials, Transportation and Environmental Engineering II |
| 编辑 | Jimmy C.M. Kao, Wen-Pei Sung, Ran Chen |
| 出版商 | Trans Tech Publications Ltd. |
| 页 | 1331-1336 |
| 页数 | 6 |
| ISBN（电子版） | 9783038352488 |
| DOI | |
| 出版状态 | 已出版 - 2014 |
| 活动 | 2nd International Conference on Materials, Transportation and Environmental Engineering, CMTEE 2014 - Kunming, 中国 期限: 30 7月 2014 → 31 7月 2014 |
出版系列
| 姓名 | Advanced Materials Research |
|---|---|
| 卷 | 1030-1032 |
| ISSN（印刷版） | 1022-6680 |
| ISSN（电子版） | 1662-8985 |
会议
| 会议 | 2nd International Conference on Materials, Transportation and Environmental Engineering, CMTEE 2014 |
|---|---|
| 国家/地区 | 中国 |
| 市 | Kunming |
| 时期 | 30/07/14 → 31/07/14 |
指纹
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Liu, R. Q., & Jiang, Y. (2014). Study on the impact of missile flight mach to its engine thrust. 在 J. C. M. Kao, W.-P. Sung, & R. Chen (编辑), Materials, Transportation and Environmental Engineering II (页码 1331-1336). (Advanced Materials Research; 卷 1030-1032). Trans Tech Publications Ltd.. https://doi.org/10.4028/www.scientific.net/AMR.1030-1032.1331