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Jet Flow Control by Dielectric Barrier Discharge: Excitation by Axisymmetric and Flapping Modes

机译：通过介电势垒放电控制射流：通过轴对称和拍击模式激励

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《AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition》|2009年|P.1-17|共17页
会议地点 Orlando FL(US)
作者
N. Benard; N. Balcon; E. Moreau;
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作者单位

LEA / University of Poitiers Chasseneuil France;

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1. Discharge-Mode Transition in Jet-Type Dielectric Barrier Discharge Using Argon/Acetone Gas Flow Ignited by Small Helium Plasma Jet [J] . Keiichiro Urabe, Keitaro Yamada, Osamu Sakai Japanese journal of applied physics . 2011,第11Issue1期

机译：小氦等离子体射流激发的氩气/丙酮气流在喷射型介质阻挡放电中的放电模式转变
2. Flow control of an elongated jet in cross-flow: Film cooling effectiveness enhancement using surface dielectric barrier discharge plasma actuator [J] . P. Audier, M. Fenot, N. Benard, Applied Physics Letters . 2016,第8期

机译：横流中细长射流的流量控制：使用表面介质阻挡放电等离子体致动器提高薄膜冷却效率
3. Lift Augmentation Based on Flap Deflection With Dielectric Barrier Discharge Plasma Flow Control Over Multi-Element Airfoils [J] . Yang Leilei, Li Jiang, Cai Jinsheng, Journal of Fluids Engineering: Transactions of the ASME . 2016,第3期

机译：基于翼片挠度的电介质阻挡放电等离子流多体机翼的升力增强
4. Jet Flow Control by Dielectric Barrier Discharge: Excitation by Axisymmetric and Flapping Modes [C] . N. Benard, N. Balcon, E. Moreau American Institute of Aeronautics and Astronautics Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition . 2009

机译：介质屏障放电喷射流量控制：轴对称和拍打模式激发
5. Modeling of Dielectric Barrier Discharge Plasma Actuators for Flow Control Simulations [D] . Palmeiro, Denis 2011

机译：介质阻挡放电等离子体致动器的流控仿真建模
6. Dissipated power and induced velocity fields data of a micro single dielectric barrier discharge plasma actuator for active flow control [O] . E. Pescini, D.S. Martínez, M.G. De Giorgi, 2015

机译：用于主动流量控制的微型单介质阻挡放电等离子体致动器的耗散功率和感应速度场数据
7. Flow control over a NACA 0012 airfoil using dielectric-barrier-discharge plasma actuator with a Gurney flap [O] . Li-Hao Feng, Timothy N. Jukes, Kwing-So Choi, 2012

机译：使用带有格尼襟翼的介质阻挡放电等离子体致动器控制NACA 0012机翼的流量

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