摘要
Gas jet of the rocket on the launch environment has serious gas shock effects, bursts of rocket impact will be greater and greater harm. This article take the numerical methods for simulation, analog transmission process gas stream flow, and finally calculate the pressure and temperature of the emitting device impingement flow field and the maximum absolute pressure and temperature, and ultimately determine gas impact of the danger zone of the flow field.
| 源语言 | 英语 |
|---|---|
| 主期刊名 | Advanced Research on Mechanical Engineering, Industry and Manufacturing Engineering III |
| 页 | 455-458 |
| 页数 | 4 |
| DOI | |
| 出版状态 | 已出版 - 2013 |
| 活动 | 2013 3rd International Conference on Mechanical Engineering, Industry and Manufacturing Engineering, MEIME 2013 - Wuhan, 中国 期限: 22 6月 2013 → 23 6月 2013 |
出版系列
| 姓名 | Applied Mechanics and Materials |
|---|---|
| 卷 | 345 |
| ISSN（印刷版） | 1660-9336 |
| ISSN（电子版） | 1662-7482 |
会议
| 会议 | 2013 3rd International Conference on Mechanical Engineering, Industry and Manufacturing Engineering, MEIME 2013 |
|---|---|
| 国家/地区 | 中国 |
| 市 | Wuhan |
| 时期 | 22/06/13 → 23/06/13 |
指纹
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Zhang, Y., Jiang, Y., & Dong, X. T. (2013). Simulation and analysis for the rocket gas flow field based on mechanical mechanics and mechanical properties. 在 Advanced Research on Mechanical Engineering, Industry and Manufacturing Engineering III (页码 455-458). (Applied Mechanics and Materials; 卷 345). https://doi.org/10.4028/www.scientific.net/AMM.345.455