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Airflow Reattachment Along a NACA 0015 Airfoil by Surfaces Dielectric Barrier Discharge Actuator: Time- Resolved Particle Image Velocimetry Investigation

机译：表面介电势垒放电促动器沿NACA 0015翼型重新附着气流：时间分辨粒子图像测速研究

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《AIAA Fluid Dynamics Conference and Exhibit》|2008年|P.1-17|共17页
会议地点 Seattle WA(US)
作者
N. Benard; P. Braud; J. Jolibois; E. Moreau;
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University of Poitiers Futuroscope France;

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1. Nanosecond-Pulsed Dielectric Barrier Discharge Plasma Actuator for Airflow Control Along an NACA0015 Airfoil at High Reynolds Number [J] . Eric Moreau, Antoine Debien, Nicolas Benard, Plasma Science, IEEE Transactions on . 2016,第11期

机译：纳秒脉冲介质阻挡放电等离子体致动器，用于沿高雷诺数的NACA0015翼型进行气流控制。
2. Application of an AC barrier discharge actuator to control airflow separation above a NACA 0015 airfoil: Optimization of the actuation location along the chord [J] . Jolibois J, Forte M, Moreau E Journal of Electrostatics . 2008,第9a10期

机译：交流障碍放电致动器在控制NACA 0015机翼上方的气流分离中的应用：沿弦的致动位置的优化
3. Flow control over a NACA 0012 airfoil using dielectric-barrier-discharge plasma actuator with a Gurney flap [J] . Li-Hao Feng, Timothy N. Jukes, Kwing-So Choi, Experiments in Fluids . 2012,第6期

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
4. Airflow Reattachment Along a NACA 0015 Airfoil by Surfaces Dielectric Barrier Discharge Actuator: Time- Resolved Particle Image Velocimetry Investigation [C] . N. Benard, P. Braud, J. Jolibois, 4th Flow Control Conference . 2008

机译：表面介电势垒放电促动器沿NACA 0015翼型重新附着气流：时间分辨粒子图像测速研究
5. Active flow control over a NACA 0015 airfoil by synthetic jet actuators [D] . Kabiri, Pooya 2012

机译：通过合成射流执行器主动控制NACA 0015机翼
6. Numerical Investigation on the Effects of Dielectric Barrier on a Nanosecond Pulsed Surface Dielectric Barrier Discharge [O] . Shen Zhang, Zhenli Chen, Binqian Zhang, 2019

机译：介电势垒对纳秒脉冲表面介电势垒放电影响的数值研究
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
8. Wing-tunnel investigation of effects of various aerodynamic balance shapes and sweepback on control-surface characteristics of semispan tail surfaces with NACA 0009, 0015, 66-009, 66(215)-014, and circular-arc airfoil sections [R] . Harper, John J 1951

机译：使用NaCa 0009,0015,66-009,66（215）-014和圆弧翼型截面的翼型隧道研究各种气动平衡形状和后掠对半边尾面控制表面特性的影响

Airflow Reattachment Along a NACA 0015 Airfoil by Surfaces Dielectric Barrier Discharge Actuator: Time- Resolved Particle Image Velocimetry Investigation

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