Characterization of Dielectric Barrier Discharge Plasma Actuators: Logarithmic Thrust-Voltage Quadratic Relationship

被引:11
作者
Ashpis, David E. [1 ]
Laun, Matthew C. [2 ]
机构
[1] NASA, John H Glenn Res Ctr, Prop Div, 21000 Brookpark Rd, Cleveland, OH 44135 USA
[2] HX5 Sierra LLC, NASA, John H Glenn Res Ctr, Facil Div, 21000 Brookpark Rd, Cleveland, OH 44135 USA
关键词
ENHANCED AERODYNAMICS; OPTIMIZATION;
D O I
10.2514/1.J055925
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Results of thrust measurements of dielectric barrier discharge plasma actuators are presented. The test setup, measurement, and data processing methodology that were developed in prior work were used. The tests were conducted with high-density polyethylene actuators of three thicknesses. The applied voltage driving the actuators was a pure sinusoidal waveform. The test setup was a suspended actuator with a decoupling liquid interface. The tests were conducted at low ambient humidity. The thrust was measured with an analytical balance and the results were corrected for antithrust to isolate the plasma-generated thrust. Applying this approach resulted in smooth and repeatable data. It also enabled precise curve fitting that yielded quadratic relations between the plasma thrust and voltage in log-log space at constant frequencies. The results contrast power law relationships developed in literature that now appear to be an approximation only over a limited voltage range.
引用
收藏
页码:3807 / 3816
页数:10
相关论文
共 21 条
[1]  
Ashpis D.E., 2013, B AM PHYS SOC, V58, P416
[2]  
Ashpis D E., 2014, 52 AER SCI M AIAA SC, DOI [10.2514/6.2014-0486, DOI 10.2514/6.2014-0486]
[3]  
Ashpis D. E., 2014, NASATM2014218115
[4]  
Baird C, 2006, AIAA paper 2006-168, DOI [10.2514/6.2006-168, DOI 10.2514/6.2006-168]
[5]  
Benard N., 2009, P 47 AIAA AER SCI M, DOI [10.2514/6.2009-488, DOI 10.2514/6.2009-488]
[6]   Electrical and mechanical characteristics of surface AC dielectric barrier discharge plasma actuators applied to airflow control [J].
Benard, Nicolas ;
Moreau, Eric .
EXPERIMENTS IN FLUIDS, 2014, 55 (11)
[7]   SDBD plasma enhanced aerodynamics: concepts, optimization and applications [J].
Corke, Thomas C. ;
Post, Martiqua L. ;
Orlov, Dmitry M. .
PROGRESS IN AEROSPACE SCIENCES, 2007, 43 (7-8) :193-217
[8]   Dielectric Barrier Discharge Plasma Actuators for Flow Control [J].
Corke, Thomas C. ;
Enloe, C. Lon ;
Wilkinson, Stephen P. .
ANNUAL REVIEW OF FLUID MECHANICS, 2010, 42 :505-529
[9]   Single dielectric barrier discharge plasma enhanced aerodynamics: physics, modeling and applications [J].
Corke, Thomas C. ;
Post, Martiqua L. ;
Orlov, Dmitriy M. .
EXPERIMENTS IN FLUIDS, 2009, 46 (01) :1-26
[10]   Evaluation of thrust measurement techniques for dielectric barrier discharge actuators [J].
Durscher, Ryan ;
Roy, Subrata .
EXPERIMENTS IN FLUIDS, 2012, 53 (04) :1165-1176