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旋成体导弹头部母线线型的选择问题研究
引用本文:唐伟,江定武,桂业伟,张瑞文.旋成体导弹头部母线线型的选择问题研究[J].空气动力学学报,2010,28(2).
作者姓名:唐伟  江定武  桂业伟  张瑞文
作者单位:中国空气动力研究与发展中心,四川,绵阳,621000
摘    要:研究旋成体导弹的头部母线线型选择确定问题。在高超声速条件下,计算并对比分析了锥形、圆弧形、抛物形、指数形和冯卡门曲线形等5种母线线型旋成体弹头的升阻特性和压心特性,并结合结构布局和分段容积要求探讨头部母线线型问题。

关 键 词:母线线型  气动特性  气动布局  总体设计  导弹  

Study on generatrix curvetypes of axis-symmetric missiles
TANG Wei,JIANG Ding-wu,GUI Ye-wei.ZHANG Rui-wen.Study on generatrix curvetypes of axis-symmetric missiles[J].Acta Aerodynamica Sinica,2010,28(2).
Authors:TANG Wei  JIANG Ding-wu  GUI Ye-weiZHANG Rui-wen
Institution:China Aerodynamics Research and Development Center/a>;Mianyang/a>;Sichuan 621000/a>;China
Abstract:Selection and confirmation of generatrix linetypes of axis-symmetric missiles are investigated.Five typical curvetypes,such as conic,arc,parabolic,exponential and Von Karmen curve,are proposed as potential axis-symmetric missile configuration generatrix line,the hypersonc aerodynamic characteristics of drag,lift-to-drag,pressure distribution and center of pressure are predicted and analyzed,and the requirments of structure and inner overall layout are discussed also.The conic body is the most steady one and...
Keywords:generatrix curvetype  aerodynamic characteristic  aerodynamic configuration  overall layout  missile  
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