Abstract
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.
| Original language | English |
|---|---|
| Title of host publication | Materials, Transportation and Environmental Engineering II |
| Editors | Jimmy C.M. Kao, Wen-Pei Sung, Ran Chen |
| Publisher | Trans Tech Publications Ltd. |
| Pages | 1331-1336 |
| Number of pages | 6 |
| ISBN (Electronic) | 9783038352488 |
| DOIs | |
| Publication status | Published - 2014 |
| Event | 2nd International Conference on Materials, Transportation and Environmental Engineering, CMTEE 2014 - Kunming, China Duration: 30 Jul 2014 → 31 Jul 2014 |
Publication series
| Name | Advanced Materials Research |
|---|---|
| Volume | 1030-1032 |
| ISSN (Print) | 1022-6680 |
| ISSN (Electronic) | 1662-8985 |
Conference
| Conference | 2nd International Conference on Materials, Transportation and Environmental Engineering, CMTEE 2014 |
|---|---|
| Country/Territory | China |
| City | Kunming |
| Period | 30/07/14 → 31/07/14 |
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Liu, R. Q., & Jiang, Y. (2014). Study on the impact of missile flight mach to its engine thrust. In J. C. M. Kao, W.-P. Sung, & R. Chen (Eds.), Materials, Transportation and Environmental Engineering II (pp. 1331-1336). (Advanced Materials Research; Vol. 1030-1032). Trans Tech Publications Ltd.. https://doi.org/10.4028/www.scientific.net/AMR.1030-1032.1331