Numerical Study of Shockwave Induced Boundary Layer Separation Control using Plasma Actuators
46th, Aerospace sciences meeting AIAA ; 2008 ; Reno, NV
2008-01-01
12 pages
Conference paper
English
Aerospace , AIAA , Aeronautics , Astronautics
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2011
|Shockwave Induced Turbulent Boundary Layer Separation Control with Plasma Actuators
British Library Conference Proceedings | 2009
|