期刊文献+

吸气式远程超声速防空导弹一体化外形设计的几个重大技术问题 被引量:3

Several important technical questions in integrated configuration design of air-breathing long-range supersonic surface-to-air missiles
下载PDF
导出
摘要 根据国外吸气式超声速战术导弹一体化外形设计取得的最新进展 ,着重分析了这类导弹外形设计的特点和技术关键 ,提出了吸气式远程超声速防空导弹一体化外形设计中应解决好的几个重大技术问题 ,以期引起各方对吸气式防空导弹总体设计中有关问题的关注和讨论 。 According to the current progress of overseas integrated configuration design of air breathing supersonic missiles,characteristic and key points of configuration design of such missiles are analyzed,as well as several important technical questions are introduced in this paper.Purpose of this paper is to raise wide dis cussion and attention about the related issues in the design of air breathing surface to air missiles and to find out an efficient way of solution.
作者 李国雄
出处 《现代防御技术》 2002年第2期29-34,43,共7页 Modern Defence Technology
关键词 吸气式 远程超声速防空导弹 一体化外形设计 吸气式导弹 进气道 气动布局 Air breathing missile Inlet Aerodynamic configuration Integrated configuration design
  • 相关文献

参考文献6

  • 1门登霍尔.战术导弹空气动力学(上)、(下)[M].洪金森等译.北京:宇航出版社,1999.
  • 2Hayes,Clyde.Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations,I--axisymmetric inlets at supersonic speeds[R].NASA-TM_84558,1983.
  • 3Hayes,Clyde.Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations,II--two-dimensional inlets at supersonic speeds[R].NASA-TM-84559,1983.
  • 4Hayes,Clyde.Aerodynamic characteristics of a series of single inlet air-breathing missile configurations[R].NASA-TM-84557,1983.
  • 5Moore M E,Jenn A A.Preliminary design aerodynamics of missile inlets[R].AIAA paper 90-3091-CP,1990.
  • 6Champigny P,Baudin D,Gonidec P.Prevision des coefficients aerodynamiques de missiles munis de prises d′air[J].Missile Aerodynamics,Oct 1990,AGARD-CP-493(AD-A238325):23-1~23-11.

同被引文献22

引证文献3

二级引证文献7

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部