Electrohydrodynamic flow control with a glow-discharge surface plasma

被引:347
作者
Roth, JR [1 ]
Sherman, DM
Wilkinson, SP
机构
[1] Univ Tennessee, Dept Elect & Comp Engn, Knoxville, TN 37996 USA
[2] Univ Tennessee, Plasma Sci Lab, Knoxville, TN 37996 USA
[3] NASA, Langley Res Ctr, Fluid Phys & Control Branch, Hampton, VA 23681 USA
关键词
Drag measurement - Glow discharge surface plasma;
D O I
10.2514/2.1110
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Multiple flow diagnostics have been applied to planar panels revered by strips of glow-discharge surface plasma in atmospheric pressure air generated by the one atmosphere uniform glow discharge plasma. Direct drag measurements, smoke wire and titanium tetrachloride Row visualization, and boundary-layer velocity profiles were obtained. The plasma generated along streamwise-oriented, symmetric strip electrodes is shown to cause a large increase in drag, whereas the plasma along spanwise-oriented, asymmetric strip electrodes can generate a significant thrust. Flow visualization and mean velocity measurements show the primary cause of the phenomena to be a combination of mass transport and vortical structures induced by strong electrohydrodynamic body forces on the Row, known as paraelectric forcing.
引用
收藏
页码:1166 / 1172
页数:7
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