High angle-of-attack calculations of the subsonic vortex flow on slender bodies

AIAA Journal ◽  
1985 ◽  
Vol 23 (8) ◽  
pp. 1150-1156 ◽  
Author(s):  
D. Almosnino
Keyword(s):  
Vortex Flow ◽  
Angle Of Attack ◽  
High Angle ◽  
High Angle Of Attack ◽  
Slender Bodies

Symmetric Vortex Separation on Circular Cylinders and Cones

1959 ◽  
Vol 26 (4) ◽  
pp. 643-648
Author(s):  
A. E. Bryson
Keyword(s):  
Unit Length ◽  
Angle Of Attack ◽  
Experimental Information ◽  
Circular Cylinders ◽  
Leeward Side ◽  
High Angle ◽  
High Angle Of Attack ◽  
Bodies Of Revolution ◽  
Vortex Separation ◽  
Slender Bodies

Abstract The symmetric vortex separation that is observed on the leeward side of slender bodies of revolution at high angle of attack in the subsonic to moderately supersonic-velocity range is analyzed by means of the “lumped-vorticity” approximation suggested by Edwards and Hill. The equivalent unsteady two-dimensional problem of indicial motion of a cylinder in an incompressible fluid with symmetric vortex wake is also considered. Body vortex position and normal force per unit length are presented for a cylinder and a slender cone at high angle of attack and compared with available experimental information.

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