| 导弹出水过程中气/水动力学的研究 |
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| 引用本文： | 罗金玲,毛鸿羽.导弹出水过程中气/水动力学的研究[J].战术导弹技术,2004,37(4):M023-25. |
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| 作者姓名： | 罗金玲 毛鸿羽 |
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| 作者单位： | 中国航天科工集团公司第三研究院,北京100074 |
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| 摘 要： | 阐述了潜射导弹头体外形的气动与水动一体化设计方法，揭示了水下运动头部产生空化的机理．根据理论与试验研究结果，分析了导弹出水过程中空泡溃灭对弹体的影响以及出水后导弹的气动特性．
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| 关 键 词： | 导弹 出水过程 气动力学 水动力学 |
| 文章编号： | 1009-1300(2004)04-0023-03 |
| 修稿时间： | 2003年12月25 |
Research on Aerodynamics and Hydrodynamics in Exiting Water Process of Missile |
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| Luo Jingling,Mao Hongyu.Research on Aerodynamics and Hydrodynamics in Exiting Water Process of Missile[J].Tactical Missile Technology,2004,37(4):M023-25. |
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| Authors: | Luo Jingling Mao Hongyu |
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| Abstract: | The integrated design method of aerodynamics and hydrodynamics of nose shape is given, an investigation on the inciption and developing cativation of nose is also obtained. According to research result of theory and experimentation, the influence of cavitation losed in exiting water process of missile as well as some aerodynamics properties of missile is analysed. |
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| Keywords: | missile exiting water process aerodynamics hydrodynamics |
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