Dielectric barrier discharge (DBD) is an active flow control device which works by ionizing the surrounding air, and controls it to achieve a desirable result. A model of the DBD has already been made, however most of them must be solved numerically. There hasn’t been any simplified non numerical model that could describe the power of a DBD. In this research, an analytical 2D equation is purposed to obtain the average velocity produced by a DBD. For validation, this equation is compared to a simulation and experimental data, which is conducted at a varying freestream velocity ranging from l to 3 m/s and also a varying dielectric thickness from 3 to 6 mm. The three of them shows good agreement on dielectric thickness of 3 mm and 4 mm with an error of 5.79% for the analytical and experimental, 2.95% for the simulation and experimental and 5.34% for the analytical and simulation. At the dielectric thickness of 6 mm some of the analytical model assumption is no longer valid, and thus a comparison couldn’t be done.

1.
Harinaldi
,
Budiarso
,
J.
Julian
, and
M. N.
Rabbani
, “
The effect of plasma actuator on the depreciation of the aerodynamic drag on box model
,”
AIP Conference Proceedings
,
1737
,
040004
, (
2016
).
2.
J.
Julian
,
Harinaldi
,
Budiarso
, “
The Effect of Plasma Actuator Utilization to the Reduction of Aerodynamic Drag of Cylinder and Box Models
,”
Proc. l2th International Conference on Heat Transfer
,
Fluid Mechanics and Thermodynamics
,
Malaga
, (
2016
).
3.
J.
Julian
,
Harniladi
,
Budiarso
,
R.
Divitro
, and
P.
Stefan
, “
The Effect of Plasma Actuator Placement on Drag Coefficient Reduction of Ahmed Body as an Aerodynamic Model
,”
International Journal of Technology
, Vol.
2
, (
2016
).
4.
D. F.
Opaits
, et al, “Surface plasma induced wall jets,”
Paper presented at 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
,
Orlando, Florida
, (
2010
).
5.
S.
Roy
and
C.-C.
Wang
, “
Numerical Investigation of Three-Dimensional Plasma Actuation for Improving Film Cooling Effectiveness
,”
Journal of Thermophysics and Heat Transfer
, Vol.
27
, No.
3
, (
2013
).
6.
K. P.
Singh
, and
S.
Roy
, “
Force approximation for a plasma actuator operating in atmospheric air
,”
Journal of Applied Physics
,
103
,
013305
, (
2008
).
7.
M.
Abdollahzadeh
,
J.
Pascoa
, and
P.
Oliveira
, “
Numerical Modeling of Boundary Layer Control Using Dielectric Barrier Discharge
,”
Paper presented at MEFTE 2012 - IV Conferencia Nacional em Mecanica dos Fluidos
,
Termodinamica e Energia
,
Lisbom, Portugal
. (
2012
).
8.
J.-S.
Yoon
and
J.-H.
Han
, “
One-equation modeling and validation of dielectric barrier discharge plasma actuator thrust
,”
J. Phys. D: Appl. Phys
,
47
,
405202
, (
2014
).
9.
A. R.
Hoskinson
,
N.
Hershkowitz
, and
D. E.
Ashpis
, “
Force measurements of single and double barrier DBD plasma actuators in quiescent air
,”
J. Phys. D: Appl. Phys
,
41
,
245209
, (
2008
).
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