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

基于CFD方法的典型防空导弹气动反设计研究
引用本文:王友进,郑咏岚,张庆兵,杨存富.基于CFD方法的典型防空导弹气动反设计研究[J].现代防御技术,2011,39(2):1-6,21.
作者姓名:王友进  郑咏岚  张庆兵  杨存富
作者单位:北京电子工程总休研究所,北京,100854
摘    要:建立了基于计算流体动力学(CFD)的防空导弹气动反设计方法,对世界几种典型防空导弹气动外形进行了反设计研究,计算了气动特性参数,进一步通过综合对比,剖析了气动布局以及气动外形的主要特点,最后给出了总结和启示,可作为工程设计的有益参考。

关 键 词:反设计  气动特性  防空导弹  计算流体动力学方法

Aerodynamic Inverse Design of Typical Air Defense Missiles Based on CFD Method
WANG You-jin,MENG Yong-lan,MANG Qing-bing,YANG Cun-fu.Aerodynamic Inverse Design of Typical Air Defense Missiles Based on CFD Method[J].Modern Defence Technology,2011,39(2):1-6,21.
Authors:WANG You-jin  MENG Yong-lan  MANG Qing-bing  YANG Cun-fu
Institution:WANG You-jin,ZHENG Yong-lan,ZHANG Qing-bing,YANG Cun-fu(Beijing Inst.of Electronic System Engineering,Beijing 100854,China)
Abstract:A method for aerodynamic inverse design of air defense missile based on computer fluid dynamics(CFD) is set up.The configuration of typical missiles in the world is investigated with the aerodynamic inverse design method and the aerodynamic characteristic parameters are calculated.Then based on integrative comparison,the main aerodynamic characteristics of the configuration and shape are analyzed.Finally,a summary and some suggestions about the research is given as useful reference for engineering design.
Keywords:inverse design  aerodynamic characteristic  air defense missile  computer fluid dynamics(CFD) method  
本文献已被 CNKI 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