Theoretical and Experimental Investigations into Vortex Flow

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Theoretical and Experimental Investigations into Vortex Flow

Theoretical and Experimental Investigations into Vortex Flow

H. W. M. Hoeijmakers / N. G. Verhaagen

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.

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Title :

Theoretical and Experimental Investigations into Vortex Flow

Contributors:

H. W. M. Hoeijmakers (author) / N. G. Verhaagen (author)

Publication date :

1985

Size :

24 pages

Type of media :

Report

Type of material :

No indication

Language :

English

Keywords :

Aircraft , Aerodynamics , Vortices , Wind tunnels , Fluid dynamics , Delta wings , Leading edges , Meetings , Foreign technology

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