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Active Control of Flow Seperation on a Swept Constant Chord Half Model in a High- Lift Configuration

机译：高升力配置中扫过恒定弦半模型流动分离的主动控制

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《American Institute of Aeronautics and Astronautics Fluid Dynamics Conference 》|2006年||共13页
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中图分类流体动力学 ;
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1. SIMULATION OF FLOW AROUND HALF-MODEL WITH HIGH-LIFT CONFIGURATION OF THE WING IN CONDITIONS OF CRYOGENIC WIND TUNNEL [J] . S.M.Bosnyakov, V.V.Vlasenko, I.A.Kursakov, TsAGI science journal . 2016 ,第1期

机译：低温风洞条件下机翼高升起时流动半周模型的模拟
2. Active Flow-Separation Control on a High-Lift Wing-Body Configuration [J] . Vlad Ciobaca, Timo Kiihn, Ralf Rudnik, Journal of Aircraft . 2013 ,第1期

机译：高提升机翼配置上的主动分流控制
3. Numerical Study of Active Flow Control on a High-Lift Configuration [J] . Tobias Hoell, Alexander Kabat vel Job, Pablo Giacopinelli, Journal of Aircraft . 2012 ,第5期

机译：高提升结构主动流控制的数值研究
4. Active Control of Flow Seperation on a Swept Constant Chord Half Model in a High- Lift Configuration [C] . R. Petz, W. Nitsche AIAA Fluid Dynamics Conference . 2006

机译：高升程配置的扫频恒定弦半模型的流分离的主动控制
5. Potential flow theory applied to lift enhancement studies and active flow control of the leading edge vortex attached to a flat plate. [D] . Mullen, Jeffrey. 2010

机译：势流理论应用于升力增强研究和主动涡流控制，该涡流附着在平板上。
6. Multi-digit coordination during lifting a horizontally oriented object: synergies control with referent configurations [O] . Yen-Hsun Wu, Vladimir M. Zatsiorsky, Mark L. Latash -1

机译：在升降水平面向对象期间的多数位协调：使用指针配置来控制协同效应
7. Investigations of active and passive flow control on civil aircraft with high-lift configuration [O] . V. G. Soudakov, A. V. Voevodin, E. E. Mamonova 2018

机译：高升力配置调查民用飞机主动和被动流量控制
8. Hinge moment and effectiveness of an unswept constant-chord control and an overhang-balanced, swept hinge-line control on an 80 degree swept pointed wing at Mach numbers from 0.75 to 1.96 [R] . Guy, Lawrence D 1956

机译：铰接力矩和有效性的未扫描恒定弦控制和悬臂平衡，扫过铰链线控制在80度扫描尖翼，马赫数从0.75到1.96

Active Control of Flow Seperation on a Swept Constant Chord Half Model in a High- Lift Configuration

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