Modern aircraft configurations derive their high-angle-of-attack capabilities to a large extent from the separation induced vortex flow from leading and side edges. In the paper theoretical and experimental investigations into vortex flow aerodynamics are described. Emphasis is placed on the description of the flow over slender highly swept wings and strake-wing configurations.
Theoretical and Experimental Investigations into Vortex Flow
1985
24 pages
Report
No indication
English
Experimental and Theoretical Investigations of a Triple Vortex Combustor with Spatial Arc
British Library Conference Proceedings | 2008
|Theoretical and experimental investigations of external turbulence effect on aircraft vortex wake
British Library Conference Proceedings | 2002
|