| 姿控发动机高空羽流流场DSMC仿真及算法研究 |
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| 引用本文： | 黄琳,任兵,吴其芬.姿控发动机高空羽流流场DSMC仿真及算法研究[J].国防科技大学学报,1998,20(3):14-17. |
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| 作者姓名： | 黄琳 任兵 吴其芬 |
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| 作者单位： | 国防科技大学航天技术系 |
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| 摘 要： | 本文分析了高空羽流流场的特性，论述了ＤＳＭＣ方法的原理以及涉及到的关键技术，应用ＤＳＭＣ方法数值求解了喷管出口附近及倒流区流场。仿真结果表明ＤＳＭＣ方法能够精确描述这一区域的流场特性。
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| 关 键 词： | 姿控发动机，高空羽流，倒流区，DSMC仿真，稀薄气体力学 |
| 收稿时间： | 1997/11/20 0:00:00 |
The Study of DSMC Method in the High-altitude Plume Flowfield of Attitude-Control Thruster |
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| Huang Lin,Ren Bing and Wu Qifen.The Study of DSMC Method in the High-altitude Plume Flowfield of Attitude-Control Thruster[J].Journal of National University of Defense Technology,1998,20(3):14-17. |
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| Authors: | Huang Lin Ren Bing and Wu Qifen |
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| Institution: | Department of Aerospace Technology, NUDT, Changsha, 410073;Department of Aerospace Technology, NUDT, Changsha, 410073;Department of Aerospace Technology, NUDT, Changsha, 410073 |
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| Abstract: | In this paper, the character of high altitude plume flowfield is analyzed. The principle of DSMC method and its key points are also discussed. Then, the flowfield of nozzle exit vicinity and backflow region are calculated by using DSMC method, The results show that with this method, the flow property of this region can be accurately described. |
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| Keywords: | attitude control thruster high altitude plume backflow region DSMC method rarefied gas dynamics |
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