DocumentCode
3329413
Title
Electrical forces in plasma actuators that result in air flow
Author
Vidmar, R.J. ; Stalder, K.R.
Author_Institution
Univ. of Nevada, Reno, NV, USA
fYear
2010
fDate
20-24 June 2010
Firstpage
1
Lastpage
1
Abstract
Air flow generated by plasma actuators is useful in modifying the boundary layer for aerodynamic purposes. In a paper by Boeuf et al a model is developed to quantify electrical forces coupled to the bulk air in a dielectric barrier discharge and estimate air flow velocity. That model is extended to include specific ion mobility and momentum transfer to the bulk gas in a plasma actuator. For regions in the actuator with high E/N and high field gradients, a dipole force is investigated. Some air species and ion species have permanent dipole moments. And, a dipole moment can be induced in atoms, molecules, and charged species that depends on the field magnitude and electronic polarizability coefficient. Ion and neutral species properties as well as the magnitude of electrical forces coupled to the bulk gas in different regions of a dielectric barrier discharge are quantified.
Keywords
discharges (electric); plasma boundary layers; plasma devices; plasma flow; aerodynamic; air flow velocity; boundary layer; dielectric barrier discharge; electrical forces; permanent dipole moments; plasma actuators; Actuators; Aerodynamics; Cities and towns; Couplings; Dielectrics; Electrohydrodynamics; Plasma properties; Polarization; USA Councils;
fLanguage
English
Publisher
ieee
Conference_Titel
Plasma Science, 2010 Abstracts IEEE International Conference on
Conference_Location
Norfolk, VA
ISSN
0730-9244
Print_ISBN
978-1-4244-5474-7
Electronic_ISBN
0730-9244
Type
conf
DOI
10.1109/PLASMA.2010.5534021
Filename
5534021
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