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  4. Investigation of Flow Separation Control by Nanosecond Pulsed Dielectric Barrier Discharge Actuators
 
book part or chapter

Investigation of Flow Separation Control by Nanosecond Pulsed Dielectric Barrier Discharge Actuators

Grech, Nadia
•
Leyland, Pénélope  
•
Peschke, Philip  
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Knight, D.
•
Lipatov, L.
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2015
Progress in Flight Physics

The ability of nanosecond pulsed DBD actuators to control flow separation was investigated on a NACA 0015 profile for velocities reaching Re = 230,000 (24 m/s). The optimal location for the actuator was determined from oil flow experiments. Moderate voltage levels were applied (3 and 6 kV) and the actuator was operated at frequencies ranging from 0.058 to 10 kHz, in pulse and burst modes. The peak effectiveness of the actuator occurred at reduced frequency values of around 1. Plasma influence was observed at all tested angles of attack (up to 26°), and the stall angle was delayed by 8°.

  • Details
  • Metrics
Type
book part or chapter
DOI
10.1051/eucass/201507191
Author(s)
Grech, Nadia
Leyland, Pénélope  
Peschke, Philip  
Ott, Peter  
Editors
Knight, D.
•
Lipatov, L.
•
Reijasse, P.
Date Issued

2015

Publisher

EUCASS, Torus Press

Publisher place

Moscow

Published in
Progress in Flight Physics
ISBN of the book

978-5-94588-165-5

Start page

191

End page

210

Series title/Series vol.

Progress in Flight Physics; 7

Volume
7
Subjects

GTT

•

LTT

•

Flow Control

•

Experimental

•

Flow Measurement

•

Plasma

Written at

EPFL

EPFL units
GTT  
Available on Infoscience
July 22, 2015
Use this identifier to reference this record
https://infoscience.epfl.ch/handle/20.500.14299/116567
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