Numerical simulation and wind tunnel testing of flutter about an all- Movable horizontal tail at transonic speeds

IMECH-IR > 流固耦合系统力学重点实验室

	Numerical simulation and wind tunnel testing of flutter about an all- Movable horizontal tail at transonic speeds
	Qian W; Yang GW(杨国伟); Zheng GN(郑冠男); Zhang GJ
会议录名称	29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
	2014
会议名称	29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
会议日期	September 7, 2014 - September 12, 2014
会议地点	St. Petersburg, Russia
摘要	In order to obtain the characteristic of flutter for a high maneuver aircraft all-movable horizontal tail, scaled structure dynamic similar models were manufactured and transonic flutter wind tunnel test was accomplished in FL-26 wind tunnel. In the mean time, CFD simulation using Navier-Stokes equation was accomplished. The horizontal tail flutter model has a rigid fuselage and a rigid wing to investigate aerodynamic influence to horizontal tail flutter boundary. Two flutter horizontal tail models were manufactured with different mass overload factor. Comparing the result of CFD simulation and wind tunnel test, a flutter design method was made for all-movable horizontal tail.
关键词	All-movable Horizontal Tail Flutter Boundaries Overload Factors Structure Dynamics Transonic Flutter Transonic Speed Wind Tunnel Tests Wind-tunnel Testing
课题组名称	LMFS流固耦合与数值计算(LHO)
ISBN号	3932182804
收录类别	EI
语种	英语
文献类型	会议论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/60233
专题	流固耦合系统力学重点实验室高温气体动力学国家重点实验室
推荐引用方式 GB/T 7714	Qian W,Yang GW,Zheng GN,et al. Numerical simulation and wind tunnel testing of flutter about an all- Movable horizontal tail at transonic speeds[C]29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014,2014.

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