Flow control over a NACA 0012 airfoil using dielectric-barrier-discharge plasma actuator with a Gurney flap (2012)
Attributed to:
Multi-projects on flow, turbulence and combustion using PIV systems
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1007/s00348-012-1263-y
Publication URI: http://dx.doi.org/10.1007/s00348-012-1263-y
Type: Journal Article/Review
Parent Publication: Experiments in Fluids
Issue: 6