Effect of Plasma Actuators on a Flat Plate Laminar Boundary Layer in Subsonic Conditions
25th, Aerodynamic measurement technology and ground testing conference ; 2006 ; San Francisco, CA
Aerodynamic measurement technology and ground testing conference ; AIAA Paper 2006-3350
01.01.2006
AIAA Paper 2006-3350
Including 25th AIAA aerodynamic measurement technology and ground testing conference 24th AIAA applied aerodynamics conference; 3rd AIAA flow control conference; 36th AIAA fluid dynamics conference and exhibit; 37th AIAA plasmadynamics and lasers conference; 9th AIAA/ASME joint thermophysics and heat transfer conference.; Paper numbers 2006-2805 to 2006-3925 with gaps held. Held on CD-ROM.; Shelved in Conference Index - see disc 11 for papers from the 25th Aerodynamic measurement technology and ground testing conference
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
FLUID DYNAMICS - Laminar Subsonic, Supersonic, and Transonic Boundary-Layer Flow past a Flat Plate
Online Contents | 2006
|STABILIZING A LAMINAR BOUNDARY-LAYER USING PLASMA-ACTUATORS
British Library Conference Proceedings | 2006
|Effect of Flat Plate Oscillation on Boundary Layer Development for Subsonic Flows
British Library Conference Proceedings | 2006
|