DocumentCode :
1885844
Title :
The effect of active manipulation of a plasma surface layer on the aerodynamic drag of a flat plate
Author :
Sherman, D.M. ; Roth ; Wilkinson, S.P.
Author_Institution :
Tennessee Univ., Knoxville, TN, USA
fYear :
1997
fDate :
19-22 May 1997
Firstpage :
230
Abstract :
Summary form only given. We report further experimental results on the aerodynamic drag of a flat panel covered with a layer of one atmosphere uniform glow discharge plasma (OAUGDP) which has been operated in the NASA-Langley Research Center´s 7/spl times/11 inch low speed wind tunnel. In particular, we hope to present results on the effects of electrode geometry, including whether there exists an optimum electrode spacing, both parallel and perpendicular to the airflow; and the first test of a flat panel in a DC accelerator configuration in which the plasma is accelerated with, against, and at right angles to the airflow.
Keywords :
aerodynamics; drag; glow discharges; plasma applications; accelerator configuration; aerodynamic drag; electrode geometry; flat panel; flat plate; one atmosphere uniform glow discharge plasma; plasma surface layer; Aerodynamics; Atmosphere; Electrodes; Geometry; Glow discharges; Life estimation; Plasma accelerators; Surface discharges; Testing; Wind speed;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Plasma Science, 1997. IEEE Conference Record - Abstracts., 1997 IEEE International Conference on
Conference_Location :
San Diego, CA, USA
ISSN :
0730-9244
Print_ISBN :
0-7803-3990-8
Type :
conf
DOI :
10.1109/PLASMA.1997.604949
Filename :
604949
Link To Document :
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