首页 | 本学科首页   官方微博 | 高级检索  
     检索      

红外空空导弹头罩热应力分析
引用本文:李建华,郭常宁,许泉,梁强.红外空空导弹头罩热应力分析[J].强度与环境,2012(2):46-52.
作者姓名:李建华  郭常宁  许泉  梁强
作者单位:1. 上海交通大学机械与动力工程学院,上海200030
2. 上海航天精密机械研究所,上海201600
3. 上海机电工程研究所,上海200233
摘    要:以红外空空弹头罩为研究对象,利用气动加热工程计算方法提供的热流密度为输入条件进行了热载状态下结构的瞬态温度场和热应力分析,并以电弧风洞试验进行验证,试验结果与计算结果吻合,表明本文方法具有一定的精度,能满足工程设计要求。利用文中的分析方法,提出降低红外头罩热应力的改进建议。

关 键 词:红外头罩  气动加热  温度场  热应力

Thermal stress analysis for the dome of the infrared air-to-air missile
LI Jianhua,GUO Changning,XU Quan,LIANG Qiang.Thermal stress analysis for the dome of the infrared air-to-air missile[J].Structure & Environment Engineering,2012(2):46-52.
Authors:LI Jianhua  GUO Changning  XU Quan  LIANG Qiang
Institution:1 School of Mechanical Engineering Shanghai Jiaotong University, Shanghai 200030, China; 2 Shanghai Space Precision Machinery Research Institute, Shanghai 201600, China 3 Shanghai Electromechanical Engineering Machinery Research Institute, Shanghai 200233, China)
Abstract:Taking the dome of infrared air-to-air missile as the research object, using the heat flux obtained by engineering calculation approach on aerodynamic heating as input condition, this paper gives a brief analysis on the instantaneous temperature field and thermal stress of missile under the hot-carrier status, and verifies it by arc wind tunnel tests. Some numerical results are in good agreements with experimental data. The result shows that accuracy of the present approach is effective for engineering application. By adopting the analysis approach of this paper, some suggestion for improvement for to reduce the thermal stress of the infrared dome was put forwarded.
Keywords:infrared dome  aero heating  temperature field  thermal stress
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号