The present work addresses the combined influence of pressure variations and different airflow velocities on the discharge intensity of plasma actuators. Power consumption, plasma length, and discharge capacitance were investigated systematically for varying pressure levels (p = 0.1–1 bar) and airflow velocities (U=0100 m/s) to characterize and quantify the favorable and adverse effects on the discharge intensity. In accordance with previous reports, an increasing plasma actuator discharge intensity is observed for decreasing pressure levels. At constant pressure levels, an adverse airflow influence on the electric actuator performance is demonstrated. Despite the improved discharge intensity at lower pressure levels, the seemingly improved performance of the plasma actuators is accompanied with a more pronounced drop of the relative performance. These findings demonstrate the dependency of the (kinematic and thermodynamic) environmental conditions on the electric performance of plasma actuators, which in turn affects the control authority of plasma actuators for flow control applications.

1.
E.
Moreau
, “
Airflow control by non-thermal plasma actuators
,”
J. Phys. D: Appl. Phys.
40
,
605
636
(
2007
).
2.
T. C.
Corke
,
C. L.
Enloe
, and
S. P.
Wilkinson
, “
Dielectric barrier discharge plasma actuators for flow control
,”
Annu. Rev. Fluid Mech.
42
,
505
529
(
2010
).
3.
L. N.
Cattafesta
and
M.
Sheplak
, “
Actuators for active flow control
,”
Annu. Rev. Fluid Mech.
43
,
247
272
(
2011
).
4.
S.
Grundmann
,
M.
Frey
, and
C.
Tropea
, “
Unmanned aerial vehicle (UAV) with plasma actuators for separation control
,” AIAA Paper 2009–698,
2009
.
5.
M. P.
Patel
,
T. T.
Ng
,
S.
Vasudevan
,
T.
Corke
,
M.
Post
,
T.
McLaughlin
, and
C. F.
Suchomel
, “
Scaling effects of an aerodynamic plasma actuator
,”
J. Aircr.
45
,
223
236
(
2008
).
6.
C. L.
Kelley
,
P. O.
Bowles
,
J.
Cooney
,
C.
He
,
T. C.
Corke
,
B. A.
Osborne
,
J. S.
Silkey
, and
J.
Zehnle
, “
Leading-edge separation control using alternating-current and nanosecond-pulse plasma actuators
,”
AIAA J.
52
(published online).
7.
S.
Im
,
H.
Do
, and
M. A.
Cappelli
, “
Dielectric barrier discharge control of a turbulent boundary layer in a supersonic flow
,”
Appl. Phys. Lett.
97
,
041503
(
2010
).
8.
P.
Gnemmi
and
C.
Rey
, “
Guidance of a supersonic projectile by a plasma-actuation concept
,” in
Wind Tunnels and Experimental Fluid Dynamics Research
(
InTech
,
2011
).
9.
R.
Anderson
and
S.
Roy
, “
Preliminary experiments of barrier discharge plasma actuators using dry and humid air
,” AIAA Paper 2006-0369,
2006
.
10.
N.
Bénard
,
N.
Balcon
, and
E.
Moreau
, “
Electric wind produced by a surface dielectric barrier discharge operating over a wide range of relative humidity
,” AIAA Paper 2009-488,
2009
.
11.
D.
Ashpis
and
M.
Laun
, “
Dielectric barrier discharge (DBD) plasma actuators thrust-measurement methodology incorporating new anti-thrust hypothesis
,” AIAA Paper 2014-0486,
2014
.
12.
D. F.
Opaits
,
G.
Neretti
,
S. H.
Zaidi
,
M. N.
Shneider
,
R. B.
Miles
,
A. V.
Likhanskii
, and
S. O.
Macheret
, “
DBD plasma actuators driven by a combination of low frequency bias voltage and nanosecond pulses
,” AIAA Paper 2008–1372,
2008
.
13.
P.
Versailles
,
V.
Gingras-Gosselin
, and
H.
Vo
, “
Impact of pressure and temperature on the performance of plasma actuators
,”
AIAA J.
48
,
859
863
(
2010
).
14.
J. W.
Gregory
,
C. L.
Enloe
,
G. I.
Font
, and
T. E.
McLaughlin
, “
Force production mechanisms of a dielectric-barrier discharge plasma actuator
,” AIAA Paper 2007-185,
2007
.
15.
Y.
Wu
,
Y.
Li
,
M.
Jia
,
H.
Song
,
Z.
Guo
,
X.
Zhu
, and
Y.
Pu
, “
Influence of operating pressure on surface dielectric barrier discharge plasma aerodynamic actuation characteristics
,”
Appl. Phys. Lett.
93
,
031503
(
2008
).
16.
N.
Bénard
,
N.
Balcon
, and
E.
Moreau
, “
Electric wind produced by a single dielectric barrier discharge actuator operating in atmospheric flight conditions-pressure outcome
,” AIAA Paper 2008-3792,
2008
.
17.
N.
Bénard
,
N.
Balcon
, and
E.
Moreau
, “
Electric wind produced by a surface dielectric barrier discharge operating in air at different pressures: aeronautical control insights
,”
J. Phys. D: Appl. Phys.
41
,
042002
(
2008
).
18.
J. A.
Valerioti
and
T. C.
Corke
, “
Pressure dependence of dielectric barrier discharge plasma flow actuators
,”
AIAA J.
50
,
1490
1502
(
2012
).
19.
T.
Nichols
and
J.
Rovey
, “
Surface potential and electric field measurements in plasma actuators at low pressures
,”
AIAA J.
51
,
1054
1065
(
2013
).
20.
T.
Abe
,
Y.
Takizawa
, and
S.
Sato
, “
Experimental study for momentum transfer in a dielectric barrier discharge plasma actuator
,”
AIAA J.
46
,
2248
2256
(
2008
).
21.
M.
Takagaki
,
S.
Isono
,
H.
Nagai
, and
K.
Asai
, “
Evaluation of plasma actuator performance in martian atmosphere for applications to mars airplanes
,” AIAA Paper 2008-3762,
2008
.
22.
G. I.
Font
,
C. L.
Enloe
,
J. Y.
Newcomb
,
A. L.
Teague
,
A. R.
Vasso
, and
T. E.
McLaughlin
, “
Effects of oxygen content on the behavior of the dielectric barrier discharge aerodynamic plasma actuator
,” AIAA Paper 2010-545,
2010
.
23.
C.
Enloe
,
J.
Baughn
,
G.
Font
, and
T.
McLaughlin
, “
Parameterization of temporal structure in the single-dielectric-barrier aerodynamic plasma actuator
,”
AIAA J.
44
,
1127
1136
(
2006
).
24.
S.
Pavon
,
J.-L.
Dorier
,
C.
Hollenstein
,
P.
Ott
, and
P.
Leyland
, “
Effects of high-speed airflows on a surface dielectric barrier discharge
,”
J. Phys. D: Appl. Phys.
40
,
1733
1741
(
2007
).
25.
K.
Barckmann
,
J.
Kriegseis
,
S.
Grundmann
, and
C.
Tropea
, “
Dielectric-barrier discharge plasmas for flow control at higher mach numbers
,” AIAA Paper 2010-4258,
2010
.
26.
J.
Kriegseis
,
S.
Grundmann
, and
C.
Tropea
, “
Airflow influence on the discharge performance of dielectric barrier discharge plasma actuators
,”
Phys. Plasmas
19
,
073509
(
2012
).
27.
J.
Kriegseis
,
A.
Duchmann
,
C.
Tropea
, and
S.
Grundmann
, “
On the classification of dielectric barrier discharge plasma actuators: A comprehensive performance evaluation study
,”
J. Appl. Phys.
114
,
053301
(
2013
).
28.
F.
Paschen
, “
Über die zum funkenübergang in luft, wasserstoff und kohlensäure bei verschiedenen drücken erforderliche potentialdifferenz
,”
Ann. Phys.
273
,
69
96
(
1889
).
29.
K.
Vollrath
, “
Funkenlichtquellen und hochfrequenz-funkenkinematographie
,” in
Kurzzeitphysik
, edited by
K.
Vollrath
and
G.
Thomer
(
Springer
,
1967
), pp.
76
165
.
30.
S.
Pavon
,
P.
Ott
,
P.
Leyland
,
J.-L.
Dorier
, and
C.
Hollenstein
, “
Effects of a surface dielectric barrier discharge on transonic flows around an airfoil
,” AIAA Paper 2009-649,
2009
.
31.
J.
Frey
, “
Dichteabhängige kalibrierung von hitzdrahtsonden im strömungskanal für verdünnte gase (Höhenwindkanal)
,” Technical Report No. 110615 (TU Dresden,
2011
).
33.
J.
Kriegseis
,
B.
Möller
,
S.
Grundmann
, and
C.
Tropea
, “
Capacitance and power consumption quantification of dielectric barrier discharge (DBD) plasma actuators
,”
J. Electrostat.
69
,
302
312
(
2011
).
34.
J.
Kriegseis
,
S.
Grundmann
, and
C.
Tropea
, “
Power consumption, discharge capacitance and light emission as measures for thrust production of dielectric barrier discharge plasma actuators
,”
J. Appl. Phys.
110
,
013305
(
2011
).
35.
T. C.
Manley
, “
The Electric characteristics of the ozonator discharge
,”
J. Electrochem. Soc.
84
,
83
96
(
1943
).
36.
V. I.
Gibalov
and
G. J.
Pietsch
, “
The development of dielectric barrier discharges in gas gaps and on surfaces
,”
J. Phys. D: Appl. Phys.
33
,
2618
(
2000
).
37.
Z.
Falkenstein
and
J. J.
Coogan
, “
Microdischarge behaviour in the silent discharge of nitrogen-oxygen and water-air mixtures
,”
J. Phys. D: Appl. Phys.
30
,
817
825
(
1997
).
38.
G.
Nersisyan
and
W. G.
Graham
, “
Characterization of a dielectric barrier discharge operating in an open reactor with flowing helium
,”
Plasma Sources Sci. Technol.
13
,
582
587
(
2004
).
39.
H. E.
Wagner
,
R.
Brandenburg
,
K. V.
Kozlov
,
A.
Sonnenfeld
,
P.
Michel
, and
J. F.
Behnke
, “
The barrier discharge: Basic properties and applications to surface treatment
,”
Vacuum
71
,
417
436
(
2003
).
40.
T.
Abe
,
Y.
Takizawa
, and
S.
Sato
, “
A parametric experimental study for momentum transfer by plasma actuator
,” AIAA Paper 2007–185,
2007
.
41.
J. R.
Hollahan
,
Techniques and Applications of Plasma Chemistry
(
John Wiley & Sons, Inc.
,
1974
).
42.
R. J.
Goldston
and
P. H.
Rutherford
,
Introduction to Plasma Physics
(
Institute of Physics Publishing
,
1995
), p.
510
.
43.
Y. P.
Raizer
, in
Gas Discharge Physics
, edited by
J. E.
Allen
(
Springer
,
1991
).
44.
J.
Kriegseis
,
D.
Schröter
,
A.
Duchmann
,
K.
Barckmann
,
S.
Grundmann
, and
C.
Tropea
, “
Closed-loop performance control of DBD plasma actuators
,”
AIAA J.
51
,
961
967
(
2013
).
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