Simulation of direct-current surface plasma discharge phenomena in high-speed flow actuation

被引:11
作者
Deconinck, Thomas [1 ]
Mahadevan, Shankar [1 ]
Raja, Laxminarayan L. [1 ]
机构
[1] Univ Texas Austin, Dept Aerosp Engn & Engn Mech, Austin, TX 78712 USA
关键词
glow discharge; high-speed flow control; self-consistent plasma simulation;
D O I
10.1109/TPS.2007.903842
中图分类号
O35 [流体力学]; O53 [等离子体物理学];
学科分类号
070204 ; 080103 ; 080704 ;
摘要
We present a self-consistent 2-D multispecies multitemperature model of dc nonequilibriurn surface plasma discharge phenomena in the presence of a low-pressure imposed high-speed convective flow. For pressures of a few torr and voltages of a few kilovolts, a nonequilibrium glow discharge is generated between the electrodes. Peak charge densities in the discharge on the order of 10(14) - 10(16) m(-3), electron temperatures on the order of 1 eV, and gas temperatures on the order of 2000 K are observed. Increasing voltages are found to increase the charge density in the discharge and also cause a constriction of the discharge volume. The same trend is also observed with an increase in the discharge pressure. The discharge is highly asymmetric owing to the high-speed convective flow, with the discharge activity restricted to the flow downstream edge of the cathode surface. The convective flow also causes a quasi-neutral plasma-tail-like feature that provides a major loss mechanism for charged and neutral species in the discharge. Despite sufficient cathode surface area, the discharge operates in an abnormal glow mode, with a positive differential resistivity, owing to a flow-induced constricted cathode attachment. Relatively large cathode sheath dimensions on the order of 1 cm are observed with a net electrostatic forcing restricted to this region. The net electrostatic forcing is largely vertical toward the cathode surface, but also has a component in the direction against the flow.
引用
收藏
页码:1301 / 1311
页数:11
相关论文
共 39 条
[1]   Plasmas in high speed aerodynamics [J].
Bletzinger, P ;
Ganguly, BN ;
Van Wie, D ;
Garscadden, A .
JOURNAL OF PHYSICS D-APPLIED PHYSICS, 2005, 38 (04) :R33-R57
[2]   A TWO-DIMENSIONAL MODEL OF DC GLOW-DISCHARGES [J].
BOEUF, JP .
JOURNAL OF APPLIED PHYSICS, 1988, 63 (05) :1342-1349
[3]   Electrohydrodynamic force and aerodynamic flow acceleration in surface dielectric barrier discharge [J].
Boeuf, JP ;
Pitchford, LC .
JOURNAL OF APPLIED PHYSICS, 2005, 97 (10)
[4]   Numerical Simulations of magnetic flow control in hypersonic chemically reacting flows [J].
Damevin, HM ;
Hoffmann, KA .
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2002, 16 (04) :498-507
[5]  
Ellis H. W., 1976, Atomic Data and Nuclear Data Tables, V17, P177, DOI 10.1016/0092-640X(76)90001-2
[6]  
Enloe CL, 2005, 43 AIAA AER SCI M EX
[7]   Boundary-layer control with atmospheric plasma discharges [J].
Font, Gabriel I. .
AIAA JOURNAL, 2006, 44 (07) :1572-1578
[8]   A high-order implicit procedure for the 3-D electric field in complex magnetogasdynamic simulations [J].
Gaitonde, DV .
COMPUTERS & FLUIDS, 2004, 33 (03) :345-374
[9]  
GAITONDE DV, 2005, 36 AIAA PLASM LAS C
[10]  
Gudmundsson J. T., 2005, RH092005 U IC SCI I