| 制导兵器气动布局发展趋势及有关气动力技术 |
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| 引用本文： | 吴甲生,雷娟棉.制导兵器气动布局发展趋势及有关气动力技术[J].北京理工大学学报,2003,23(6):665-670. |
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| 作者姓名： | 吴甲生 雷娟棉 |
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| 作者单位： | 北京理工大学,机电工程学院,北京,100081 |
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| 基金项目： | 国家部委预研基金;4013130302; |
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| 摘 要： | 论述了反坦克导弹、制导航弹、末制导炮弹、制导火箭等制导兵器常用的气动布局和特点；分析了制导兵器的新型气动布局及特点；论述了制导兵器的发展趋势是远射程、高机动、高精度、大威力和高隐身；指出了制导兵器发展中必须研究解决的关键气动力技术问题。
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| 关 键 词： | 制导兵器 气动布局 气动特性 滑翔增程 气动弹性 锥形运动 |
| 文章编号： | 1001-0645(2003)06-0665-06 |
| 收稿时间： | 2003/8/25 0:00:00 |
| 修稿时间： | 2003年8月25日 |
Trends in the Development of Aerodynamic Configuration of Guided Weapons and Relevant Aerodynamic Techniques |
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| WU Jia-sheng and LEI Juan-mian.Trends in the Development of Aerodynamic Configuration of Guided Weapons and Relevant Aerodynamic Techniques[J].Journal of Beijing Institute of Technology(Natural Science Edition),2003,23(6):665-670. |
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| Authors: | WU Jia-sheng and LEI Juan-mian |
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| Institution: | School of Mechatronics Engineering, Beijing Institute of Technology, Beijing100081, China;School of Mechatronics Engineering, Beijing Institute of Technology, Beijing100081, China |
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| Abstract: | Aerodynamic configurations in general use and aerodynamic characteristics of guided weapons, e.g. of antitank missiles, guided bombs, terminally guided projectiles, guided rockets etc., are summarized. Some new aerodynamic configurations of guided weapons and correspond-ing characteristics are analyzed. It is shown that the trends of development in guided weapons are toward long range, high maneuverability, high accuracy, high power and high stealthy. The key aerodynamic techniques to be predetermined during the development of guided weapons are pointed out and discussed. |
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| Keywords: | guided weapons aerodynamic configuration aerodynamic characteristics extended gliding range aeroelasticity conical motion |
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