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| 弹翼部件巡航状态受力分析 | |
| 引用本文： | 刘彦臣,关世玺,李战芬,李迎飞. 弹翼部件巡航状态受力分析[J]. 弹箭与制导学报, 2009, 29(3) |
| 作者姓名： | 刘彦臣 关世玺 李战芬 李迎飞 |
| 作者单位： | 1. 中北大学机电工程学院,太原,030051 2. 太原工业学院,太原,030008 3. 山西阳煤丰喜肥业(集团)股份有限公司,山西运城,044000 |
| 摘 要： | 研究了某类型弹翼部件在巡航状态下的应力、应变状况.先建立弹翼三维实体模型,并利用计算机仿真技术,加载了弹翼在巡航过程中所受到的各种载荷.然后采用有限元分析的方法,得到弹翼在巡航状态下的应力、应变数据,验证了弹翼结构设计的合理性,进而为弹翼翼型参数的研究提供依据. |
| 关 键 词： | 弹翼 受力分析 有限元分析 计算机仿真 |
Stress Analysis of Missile Wing under the Condition of Cruise |
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| LIU Yanchen,GUAN Shixi,LI Zhanfen,LI Yingfei. Stress Analysis of Missile Wing under the Condition of Cruise[J]. Journal of Projectiles Rockets Missiles and Guidance, 2009, 29(3) | |
| Authors: | LIU Yanchen GUAN Shixi LI Zhanfen LI Yingfei |
| Affiliation: | LIU Yanchen1,GUAN Shixi1,LI Zhanfen2,LI Yingfei3 (1 School of Mechatronics Engineering,North University of China,Taiyuan 030051,China,2 Taiyuan Institute of Technology,Taiyuan 030008,3 Shanxi Yangmei Fengxi Fertilizer Industry(Group)Ltd.,Shanxi Yuncheng 044000,China) |
| Abstract: | The stress strain condition of certain kinds of missile wings under the condition of cruise was studied.The data of stress strain was obtained by simulating all kinds of loads on the three-dimensional model structure of missile wings under the cruising condition.Then,the finite element analysis was employed.The purpose of the paper is to analyze whether the structure of missile wings meets the requirements of design and provide the basis for parameter study of missile wings. |
| Keywords: | missile wing stress analysis finite element analysis computer simulation |
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