弹翼部件巡航状态受力分析  

Stress Analysis of Missile Wing under the Condition of Cruise

作　　者：刘彦臣[1] 关世玺[1] 李战芬[2] 李迎飞 

机构地区：[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

出　　处：《弹箭与制导学报》2009年第3期90-92,共3页Journal of Projectiles,Rockets,Missiles and Guidance

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。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.

关 键 词：弹翼 受力分析 有限元分析 计算机仿真 

分 类 号：TJ760.34[兵器科学与技术—武器系统与运用工程]