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

飞机横-航向耦合模态特性和飞行品质优化研究
引用本文:郑本武,夏伟国.飞机横-航向耦合模态特性和飞行品质优化研究[J].飞行力学,1991(4).
作者姓名:郑本武  夏伟国
作者单位:南京航空学院,南京航空学院
摘    要:本文阐述了飞机横—航向耦合的形成机理,研究了气动外形参数变化对滚转-螺旋耦合模态的影响。文中提出对横—航向模态特性进行优化的算法,该算法对飞机的改型和初步设计有一定的参考价值。最后对某歼击机的横—航向模态特性进行了优化计算,计算结果表明,该机在许多状态下的飞行品质得到了提高。

关 键 词:横—航向耦合  滚转—螺旋耦合模态  横—航向模态特性

INVESTIGATION OF THE LATERAL DIRECTIONAL COUPLING MODES OF AIRCRAFT AND OF OPTIMIZATION OF FLYING QUALITIES
Zheng Benwu,Xia Weiguo.INVESTIGATION OF THE LATERAL DIRECTIONAL COUPLING MODES OF AIRCRAFT AND OF OPTIMIZATION OF FLYING QUALITIES[J].Flight Dynamics,1991(4).
Authors:Zheng Benwu  Xia Weiguo
Institution:Nanjing Aeronaticat Institute
Abstract:This paper describes the mechanism of the lateral-directional coupling formation of aircraft and investigates the influence of geometric parameters of aircraft on coupled roll-spiral mode. A method of optimizing the lateral-directional modes is presented in this paper. This optimization method is useful for initial design and reformation of aircraft. These lateral-directional modes are calculated by using optimization techniques. The results indicate that the flying qualities have been improved in many flight conditions.
Keywords:lateral-directional coupling  coupled roll-spiralmode  lateral-directional modes  
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