期刊文献+

一种飞翼布局横航向特性的控制研究 被引量:6

An investigation on controlling lateral characteristics for a flying wing configuration
下载PDF
导出
摘要 给出了在一种飞翼布局上多种气动措施对该布局航向特性影响的探索性研究,包括机头安装不对称边条,机翼前缘不对称安装绕流物以及机头不同位置微量吹气等。结果表明这些措施都能提供航向控制力矩,其中头部边条的作用最明显,头部不对称切向吹气提供的航向控制能力也能达到常规方向舵的水平。 An exploratory investigation to the effects of some aerodynamic devices including asymmetric nose strake, asymmetric spoiler on leading edge of wing, and weak blowing on nose of fuselage,is given in the paper.The results shown that these devices all can provide moment for yawing control, especially the nose strake with appreciable effects, and the yawing control capability provided by asymmetric nose blowing in tangent direction can reach the level provided by convention rudder.
作者 赵霞 秦燕华
出处 《空气动力学学报》 CSCD 北大核心 2008年第2期234-238,共5页 Acta Aerodynamica Sinica
关键词 飞翼布局 大攻角空气动力 切向吹气 flying wing aerodynamics of high angle of attack tangent blowing
  • 相关文献

参考文献7

  • 1KENNETH P, IWANSKI MATTHEW J O' ROURKE. F-15 forebody vortex flow control using jet nozzle blowing[R] .AIAA-95- 1800-CP.
  • 2MATTHEW J O' ROURKE. Experimental investigation of slot blowing for yaw control on a generic fighter configuration with a chined forebedy[ R]. AIAA-95-1798-CP.
  • 3MATTHEW J O ' Rouke , JENNIFER L SEDOR . Forebedy - mounted jet nozzles for yaw control on a generic fighter configuration with a chined forebedy[ R]. AIAA-95-3490-CP.
  • 4DAVID R WILLIAMS. A review of forebody vortex control scenarios[ R]. AIAA-1997-1967.
  • 5MATTHEW J.O' ROURKE,JOHN N R,STEFAN J K,KEVIN J L. Development of a conformal pneumatic forebody control for next-generation rioters[ R] . AIAA-1996-786.
  • 6CRAIG A Hunter, Sally A V,BICHAD M W,STEVEN X S B. Advanced aerodynamic design of passive porosity control effectots[ R]. AIAA 2001-0249.
  • 7FREDERICK W R. Micro-blowing for high-angle-of-attack vortex flow control on a fighter aircraft [ J ]. Journal of Aircraft, 2001,38(3) :454-457.

同被引文献40

引证文献6

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