Numerical simulation and wind tunnel testing of flutter about an all- Movable horizontal tail at transonic speeds
文献类型：会议论文
| 作者 | Qian W; Yang GW(杨国伟) ; Zheng GN(郑冠男); Zhang GJ
|
| 出版日期 | 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 |
| 关键词 | All-movable horizontal tail Flutter boundaries Overload factors Structure dynamics Transonic flutter Transonic speed Wind tunnel tests Wind-tunnel testing |
| 中文摘要 | 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. |
| 收录类别 | EI |
| 会议录 | 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
 |
| 语种 | 英语 |
| ISBN号 | 3932182804 |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/60233]  |
| 专题 | 力学研究所_流固耦合系统力学重点实验室(2012-) 力学研究所_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]. 见:29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014. St. Petersburg, Russia. September 7, 2014 - September 12, 2014. |
入库方式： OAI收割
来源：力学研究所
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