AIAA 2006-1058 Numerical Study of Aerodynamic Performance of Airfoils at Low Angles of Attack by Active Flow Control of Trailing Edge Vortices
44th, Aerospace sciences meeting ; 2006 ; Reno, NV
Aerospace sciences meeting ; 12702-12721
2006-01-01
20 pages
VOL 17 of 24 VOLS
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Aerodynamic Performance Modification at Low Angles of Attack by Trailing Edge Vortices
British Library Conference Proceedings | 2004
|Aerodynamic Performance of Thick Blunt Trailing Edge Airfoils
British Library Conference Proceedings | 2010
|