Published February 21, 2008 | Version v1
Journal article

Electric wind produced by a surface dielectric barrier discharge operating in air at different pressures: aeronautical control insights

  • 1. Laboratoire d'Etudes Aerodynamiques (LEA), Universite de Poitiers, ENSMA, CNRS Bld Marie et Pierre Curie, Teleport 2, 86962 Futuroscope Cedex (France)

Description

The effects of the ambient air pressure level on the electric wind produced by a single dielectric barrier discharge (DBD) have been investigated by Pitot velocity measurements. Pressures from 1 down to 0.2 atm were tested with a 32 kVp-p 1 kHz excitation. This preliminary study confirms the effectiveness of surface DBD at low pressure. Indeed, the induced velocity is strongly dependent on the ambient air pressure level. Quite surprisingly the produced airflow presents a local maximum at 0.6 atm. The measured velocities at 1 atm and 0.2 atm are 2.5 m s-1 and 3 m s-1, respectively while 3.5 m s-1 is reached at 0.6 atm. The position of the maximal velocity always coincides with the plasma extension. Mass flow rate calculations indicate that the DBD is effective in real flight pressure conditions. (fast track communication)

Availability note (English)

Available from http://dx.doi.org/10.1088/0022-3727/41/4/042002

Additional details

Identifiers

DOI
10.1088/0022-3727/41/4/042002;
PII
S0022-3727(08)67114-4;

Publishing Information

Journal Title
Journal of Physics. D, Applied Physics
Journal Volume
41
Journal Issue
4
Journal Page Range
[5 p.]
ISSN
0022-3727
CODEN
JPAPBE

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
40060966
Subject category
S71: CLASSICAL AND QUANTUM MECHANICS, GENERAL PHYSICS;
Descriptors DEI
AIR; DIELECTRIC MATERIALS; FLOW RATE; MASS; PLASMA; VELOCITY
Descriptors DEC
FLUIDS; GASES; MATERIALS