Flow control over a NACA 0012 airfoil using dielectric-barrier-discharge plasma actuator with a Gurney flap (2012)

First Author: Feng L

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