Semi-active Control Wind Tunnel Tests of Wing/store System Flutter with an Electro-Magnetic damper

机译：用电磁阻尼器翼/储存系统扑振的半主动控制风隧道试验

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Wind tunnel tests of wing/store system flutter semi-active suppression are shown in this paper. A wind tunnel test model for semi-active suppression with an Electro-Magnetic damper and circuit control system are designed and worked out. The results of these wind tunnel tests show that the flutter response of wing/store system can be suppressed and the method of the tests is reasonable.

机译：本文示出了翼/储存系统颤动半主动抑制的风洞试验。设计并制定了具有电磁阻尼器和电路控制系统的半主动抑制的风洞试验模型。这些风洞测试的结果表明，可以抑制翼/储存系统的颤动响应，并且测试方法是合理的。

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《SEM Annual Conference Exposition on Experimental and Applied Mechanics》|2003年||共6页
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Hu Weibing; Li Lizhou;
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中图分类 O39-53;
关键词
Wind tunnel test; Electro-magnetic damper; Semi-active suppression;

机译：风隧道试验;电磁阻尼器;半主动抑制;

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专利

1. KBM METHOD OF ANALYZING LIMIT CYCLE FLUTTER OF A WING WITH AN EXTERNAL STORE AND COMPARISON WITH A WIND-TUNNEL TEST [J] . Yang YR. Journal of Sound and Vibration . 1995,第2期

机译：KBM法分析带外壁机翼的极限振颤并与风洞试验比较
2. Design of active flutter suppression and wind-tunnel tests of a wing model involving a control delay [J] . Huang Rui, Qian Wenmin, Hu Haiyan, Journal of Fluids and Structures . 2015,第Null期

机译：具有控制延迟的机翼模型的主动颤振抑制设计和风洞测试
3. Design of aeroelasticity bench test for NACA0012 wing model in the low speed wind tunnel: Influence of wing's parameters on flutter speed [J] . Thi Tuyet Nhung Le, Chi-Cong Nguyen, Hoang Nam Vang International Journal of Mechanical Engineering and Applications . 2015,第1a3期

机译：低速风洞中NACA0012机翼模型的空气弹性台架试验设计：机翼参数对扑扑速度的影响
4. Semi-active Control Wind Tunnel Tests of Wing/store System Flutter with an Electro-Magnetic damper [C] . Hu Weibing, Li Lizhou Proceedings of the 2003 SEM annual conference amp; exposition on experimental and applied mechanics . 2003

机译：带有电磁阻尼器的机翼/存储系统颤振的半主动控制风洞测试
5. Design, Development and Tests in Real Time of Control Methodologies for a Morphing Wing in Wind Tunnel = [D] . Tchatchueng Kammegne, Michel Joel. 2016

机译：风洞中变形翼的控制方法的实时设计，开发和测试=
6. Fuzzy Logic-Based Control for a Morphing Wing Tip Actuation System: Design Numerical Simulation and Wind Tunnel Experimental Testing [O] . Shehryar Khan, Teodor Lucian Grigorie, Ruxandra Mihaela Botez, 2019

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7. DEVELOPMENT OF WIND TUNNEL TEST SYSTEM CONSIDERING PASSIVE CONTROL OF TALL BUILDING AND FUNDAMENTAL STUDY ON WIND RESPONSE : Wind tunnel tests of tall building having viscous or visco-elastic damper under uniform flow [O] . Daiki SATO, Kazuhiko KASAI, Tetsuro TAMURA 2006

机译：考虑高层建筑被动控制的风洞试验系统的开发与风响应基本研究：均匀流动下粘性或粘弹性阻尼器的高层建筑风隧道试验
8. Wind-Tunnel Tests on the Effects of an Added Mass on the Flutter of a Model Delta Wing PartⅠ. Fixed Root Flutter Tests PartⅡ. Anti-Symmetric Flutter Tests PartⅢ. Symmetric Flutter Tests [R] . H. HALL, W. A. COLES 1962

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Semi-active Control Wind Tunnel Tests of Wing/store System Flutter with an Electro-Magnetic damper

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