Flow control for unmanned air vehicles

D Greenblatt, DR Williams - Annual Review of Fluid Mechanics, 2022 - annualreviews.org
The pervasiveness of unmanned air vehicles (UAVs), from insect to airplane scales,
combined with active flow control maturity, has set the scene for vehicles that differ markedly …

[HTML][HTML] Exploration and outlook of plasma-actuated gas dynamics

LI Yinghong, WU Yun, L Hua, ZHU Yifei, Z Haideng… - 力学进展, 2022 - lxjz.cstam.org.cn
Plasma-actuated gas dynamics is an inter-discipline that concerns both the force and flow
characteristics of an object submerged in flow, and the internal flow characteristics under the …

High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator

J Little, M Nishihara, I Adamovich, M Samimy - Experiments in fluids, 2010 - Springer
Control of flow separation from the deflected flap of a high-lift airfoil up to Reynolds numbers
of 240,000 (15 m/s) is explored using a single dielectric barrier discharge (DBD) plasma …

Flow control on a high-lift wing with microsecond pulsed surface dielectric barrier discharge actuator

B Wei, Y Wu, H Liang, Z Su, Y Li - Aerospace Science and Technology, 2020 - Elsevier
In this study, microsecond pulsed surface dielectric barrier discharge (mSDBD) is utilized to
improve the aerodynamic characteristics of a high-lift wing. First, the characteristics of the …

Aerodynamic modification of NACA 0012 airfoil by trailing-edge plasma gurney flap

PF Zhang, AB Liu, JJ Wang - Aiaa Journal, 2009 - arc.aiaa.org
The effect of a novel plasma Gurney flap on the aerodynamic characteristics of a NACA
0012 airfoil is studied by solving the Reynolds-averaged Navier–Stokes equations. The …

Heat transfer characteristics of plasma actuation in different boundary-layer flows

W Hui, H Zhang, J Wang, X Meng, H Li - Physics of Fluids, 2022 - pubs.aip.org
The coupling characteristics of the aerodynamic and thermal effects of a surface dielectric
barrier discharge plasma actuator and its transfer characteristics in different boundary-layer …

[HTML][HTML] 等离子体激励气动力学探索与展望

李应红, 吴云, 梁华, 朱益飞, 张海灯, 郭善广 - 力学进展, 2022 - lxjz.cstam.org.cn
等离子体激励气动力学是研究等离子体激励与流动相互作用下, 绕流物体受力和流动特性以及
管道内部流动规律的科学, 属于空气动力学, 气体动力学与等离子体动力学交叉前沿领域 …

[HTML][HTML] Aerodynamic performance enhancement of a flying wing using nanosecond pulsed DBD plasma actuator

M Han, J Li, Z Niu, H Liang, G Zhao, W Hua - Chinese Journal of …, 2015 - Elsevier
Experimental investigation of aerodynamic control on a 35° swept flying wing by means of
nanosecond dielectric barrier discharge (NS-DBD) plasma was carried out at subsonic flow …

Experimental study of plasma flow control on highly swept delta wing

PF Zhang, JJ Wang, LH Feng, GB Wang - AIAA journal, 2010 - arc.aiaa.org
AERODYNAMIC flow control based on plasma actuators is now in expansion, because
plasma actuators are fully electronic with no moving parts; they have an extremely fast …

Numerical simulation on plasma circulation control airfoil

PF Zhang, B Yan, AB Liu, JJ Wang - AIAA journal, 2010 - arc.aiaa.org
CIRCULATION control (CC) concept is inspired by the well known Coanda effect, invented
by Romanian inventor Henri Coanda in early 1930s [1]. It means the tendency offluids to …