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飞翼布局无人航空器气动特性研究
引用本文:刘超,黄俊,吴洋.飞翼布局无人航空器气动特性研究[J].飞机设计,2009,29(1).
作者姓名:刘超  黄俊  吴洋
作者单位:北京航空航天大学,航空科学与工程学院,北京,100191
摘    要:飞翼布局飞机取消了尾翼,拥有良好的气动、隐身特性,但操纵效率有所下降,需要在飞机设计过程中合理地布置操纵面,改善飞翼飞机在操纵性能上的缺陷,因此,飞翼飞机的操纵面不仅要提供足够的控制力,同时还要满足飞机的稳定性要求.对飞翼布局飞机的气动特性和基本操稳特性做理论分析,并利用试验做实际对比,研究飞机的气动特性,分析各操纵面的功能、操纵特性以及存在的问题,为增强飞机稳定性和设计增稳系统增加依据.

关 键 词:飞翼布局  稳定性  气动特性  操稳特性  增稳系统

Aerodynamics Characteristics Investigation for Flying Wing Uninhabited Aircraft
LIU Chao,HUANG Jun,WU Yang.Aerodynamics Characteristics Investigation for Flying Wing Uninhabited Aircraft[J].Aircraft Design,2009,29(1).
Authors:LIU Chao  HUANG Jun  WU Yang
Institution:School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;Beijing 100191;China
Abstract:Flying wing configuration aircraft gets rid of tail in order to improve aerodynamics characteristic and reduces RCS(Radar Cross Section),but it also leads to the reduction of controlling efficiency.Control surfaces play an important role in the design of flying wing configuration aircraft.The logical control surfaces can ameliorate the limitation,provide enough control strength,and satisfy the requirement of the stability of flying wing aircraft.Aerodynamics characteristics and elementary stability and cont...
Keywords:flying wing configuration  stability  aerodynamics characteristics  stability and control  stability augmentation system  
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