飞翼布局在无人侦察作战飞机上的应用探讨  

Application of Flying Wing Configuration to UCAV for Reconnaissance

作　　者：詹光[1] 刘艳华[1] 

机构地区：[1]沈阳飞机设计研究所,辽宁沈阳110035

出　　处：《飞机设计》2007年第5期7-11,共5页Aircraft Design

摘　　要：从飞翼布局的特点出发,分析将飞翼布局应用于无人侦察作战飞机的优势,并探讨了将飞翼布局在应用中引入的几个主要技术问题。最后,指出飞翼布局是无人侦察作战飞机气动布局的较好选择。Advantages in application of flying wing configuration to UCAV for reconnaissance are analyzed. Some major technical issues resulting from the application of flying wing configuration are discussed. Finally, it is suggested that the flying wing configuration is an optimal selection of aerodynamic configuration design of an UCAV for reconnaissance.

关 键 词：气动布局 无人作战飞机 飞翼 

分 类 号：V221.3[航空宇航科学与技术—飞行器设计]