Reduction of Vibrations due to Dynamic Stall in Helicopters using an Actively Controlled Flap

机译：使用主动控制襟翼减少直升机动态失速引起的振动

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《43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference ; 10th AIAA/ASME/AHS Adaptive Structures Conference ; 4th AIAA Non-Deterministic Approaches Forum ; 3rd AIAA Gossamer Spacecraft Forum》|2002年|P.1-14|共14页
会议地点 Denver CO(US);Denver CO(US);Denver CO(US);Denver CO(US)
作者
G. Depailler; P. Friedmann;
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University of Michigan, Ann Arbor, MI;

University of Michigan, Ann Arbor, MI;

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原文格式 PDF
正文语种
中图分类结构力学;
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1. Rotor Performance Enhancement And Vibration Reduction In Presence Of Dynamic Stall Using Actively Controlled Flaps [J] . Li Liu, Peretz P, Friedmann, Journal of the American Helicopter Society . 2008,第4期

机译：使用主动控制襟翼在动态失速条件下提高转子性能并减少振动
2. Application of a New Compressible Time Domain Aerodynamic Model to Vibration Reduction in Helicopters Using an Actively Controlled Flap [J] . Timothy F. Myrtle, Peretz P. Friedmann Journal of the American Helicopter Society . 2001,第1期

机译：新型可压缩时域气动模型在主动减振襟翼直升机减振中的应用
3. Identification of flap motion parameters for vibration reduction in helicopter rotors with multiple active trailing edge flaps [J] . Ugur Dalli, Sefaatdin Yiiksel Shock and vibration . 2011,第5期

机译：识别具有多个主动后缘襟翼的直升机旋翼减振的襟翼运动参数
4. Reduction of Vibrations due to Dynamic Stall in Helicopters using an Actively Controlled Flap [C] . American Institute of Aeronautics and Astronautics/American Society of Mechanical Engineers/American Society of Civil Engineers/American Helicopter Society/ASC Structures, Structural Dynamics, and Materials Conference . 2002

机译：由于使用积极控制的襟翼直升机的动态失速而降低振动
5. Alleviation of dynamic stall induced vibrations in helicopter rotors using actively controlled flaps. [D] . Depailler, Gilles. 2002

机译：使用主动控制襟翼减轻直升机旋翼中的动态失速感应振动。
6. Reduction of the Radiating Sound of a Submerged Finite Cylindrical Shell Structure by Active Vibration Control [O] . Heung Soo Kim, Jung Woo Sohn, Juncheol Jeon, 2013

机译：通过主动振动控制降低水下圆柱壳结构的辐射声
7. REDUCTION OF VIBRATIONS DUE TO DYNAMIC STALL IN HELICOPTERS USING AN ACTIVELY CONTROLLED FLAP [O] . G. Depailler, P. P. Friedmann 2014

机译：使用活动控制的皮瓣减少直升机动态失速引起的振动
8. Vibration reduction in helicopter rotors using an actively controlled partial span trailing edge flap located on the blade [R] . Millott, T. A., Friedmann, P. P. 1994

机译：使用位于叶片上的主动控制的部分跨度后缘襟翼减少直升机旋翼的振动

Reduction of Vibrations due to Dynamic Stall in Helicopters using an Actively Controlled Flap

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