Force interaction of high pressure glow discharge with fluid flow for active separation control

被引:19
作者
Roy, S [1 ]
Gaitonde, DV
机构
[1] Kettering Univ, Compuat Plasma Dynam Lab, Flint, MI 48504 USA
[2] USAF, Computat Sci Branch, Air Vehicle Directorate, Res Lab, Wright Patterson AFB, OH 45433 USA
关键词
D O I
10.1063/1.2168404
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
Radio frequency based discharges at atmospheric pressures are the focus of increased interest in aerodynamics because of the wide range of potential applications including, specifically, actuation in flows at moderate speeds. Recent literature describing promising experimental observations, especially on separation control, has spurred efforts in the development of parallel theoretical modeling to lift limitations in the current understanding of the actuation mechanism. The present effort demonstrates higher fidelity first-principle models in a multidimensional finite-element framework to predict surface discharge-induced momentum exchange. The complete problem of a dielectric barrier discharge at high pressure with axially displaced electrodes is simulated in a self-consistent manner. Model predictions for charge densities, the electric field, and gas velocity distributions are shown to mimic trends reported in the experimental literature. Results show that a residual of electrons remains deposited on the dielectric surface downstream of the exposed powered electrode for the entire duration of the cycle and causes a net electric force in the direction from the electrode to the downstream surface. For the first time, results document the mitigation process of a separation bubble formed due to flow past a flat plate inclined at 12 S angle of attack. This effort sets the basis for extending the formulation further to include polyphase power input in multidimensional settings, and to apply the simulation method to flows past common aerodynamic configurations. (c) 2006 American Institute of Physics.
引用
收藏
页数:11
相关论文
共 29 条
[1]   Plasma interferometry at high pressures [J].
Akhtar, K ;
Scharer, JE ;
Tysk, SM ;
Kho, E .
REVIEW OF SCIENTIFIC INSTRUMENTS, 2003, 74 (02) :996-1001
[2]   Design sensitivity analysis and optimization of steady fluid-thermal systems [J].
Balagangadhar, D ;
Roy, S .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2001, 190 (42) :5465-5479
[3]   Gas discharge plasmas and their applications [J].
Bogaerts, A ;
Neyts, E ;
Gijbels, R ;
van der Mullen, J .
SPECTROCHIMICA ACTA PART B-ATOMIC SPECTROSCOPY, 2002, 57 (04) :609-658
[4]   Gas transport characteristics through a carbon nanotubule [J].
Cooper, SM ;
Cruden, BA ;
Meyyappan, M ;
Raju, R ;
Roy, S .
NANO LETTERS, 2004, 4 (02) :377-381
[5]  
CORKE T, 2002, P 43 AER SCI M REN 2
[6]  
CORKE TC, 2002, 40 AIAA AER SCI M RE
[7]   Mechanisms and responses of a single dielectric barrier plasma actuator: Geometric effects [J].
Enloe, CL ;
McLaughlin, TE ;
VanDyken, RD ;
Kachner, KD ;
Jumper, EJ ;
Corke, TC ;
Post, M ;
Haddad, O .
AIAA JOURNAL, 2004, 42 (03) :595-604
[8]  
GAITONDE D, 2002, 36 AIAA PLASM DYN LA
[9]  
GAITONDE D, 2002, P 43 AER SCI M REN 2
[10]  
JACOB JD, 2005, 4 INT S TURB SHEAR F