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

弹道靶中超高速发射弹的流场及空气动力特性研究(英)
引用本文:P.I.科瓦廖夫!俄罗斯,A.N.米哈列夫!俄罗斯,A.B.鲍德拉斯金!俄罗斯,S.G.汤姆森!俄罗斯,V.A希里亚耶夫!俄罗斯,S.A.伊萨耶夫!俄罗斯.弹道靶中超高速发射弹的流场及空气动力特性研究(英)[J].实验流体力学,1999(3).
作者姓名:P.I.科瓦廖夫!俄罗斯  A.N.米哈列夫!俄罗斯  A.B.鲍德拉斯金!俄罗斯  S.G.汤姆森!俄罗斯  V.A希里亚耶夫!俄罗斯  S.A.伊萨耶夫!俄罗斯
作者单位:圣彼得堡工学院(P.I.科瓦廖夫!俄罗斯,A.N.米哈列夫!俄罗斯,A.B.鲍德拉斯金!俄罗斯,S.G.汤姆森!俄罗斯,V.A希里亚耶夫!俄罗斯),圣彼得堡民航学院(S.A.伊萨耶夫!俄罗斯)
摘    要:本文描述的是研究爆炸成型发射弹(EFP)模型的流场及超高速空气动力特性所用的弹道试验设备;简要报导了记录全尺寸干涉图形的技术;对径向密度分布再现的方法进行了讨论;在零攻角实验时不同模型的空气动力阻力是采用简化方法来计算的;对各种不同EFP型式的气动稳定性提出了定性估计的方法;并阐述了用于组合体超高速飞行特性研究的数值计算技术的基本原理

关 键 词:超高速  爆炸成型发射弹  弹道靶  流动干涉图  空气动力系数

The investigation of the aerodynamic properties and flow field of the hyperve locity projectiles at the ballistic range
P.I.Kovalev,A.N.Mikhalev,A.B.Podlaskin,S.G.Thomson,V.A.Shiriaev.The investigation of the aerodynamic properties and flow field of the hyperve locity projectiles at the ballistic range[J].Experiments and Measur in Fluid Mechanics,1999(3).
Authors:PIKovalev  ANMikhalev  ABPodlaskin  SGThomson  VAShiriaev
Abstract:The range equipment for the investigation of the hypervelocity aerodynamic properties and flow field of explosively formed projectile(EFP) models is described.The technique of the full scale interferogram recording is briefly reported.The procedure of the radial density distributions reconstruction is discussed.The aerodynamic drag of different models at zero angle of attack in the experiment is calculated using the simplified procedure.The qualitative considerations about aerodynamic stability for various EFP forms are proposed.The fundamentals of the numerical calculation technique applied to research of hypervelosity flight characteristics of composed bodies are formulated.
Keywords:hypervelocity  explosively formed projectile  ballistic range  flow interferogram  aerodynamical coefficients  
本文献已被 CNKI 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