Change of asymmetric vortex-flow pattern as function of reynolds number and incidence behind circular cone

21st Atmospheric Flight Mechanics Conference

Volumn , Issue , 1996, Pages 240-245

  Stahl, W H ^a   Asghar, A ^a  

^a KING FAHD UNIVERSITY OF PETROLEUM AND MINERALS   (Saudi Arabia)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; FLOW PATTERNS; LAMINAR FLOW; REYNOLDS NUMBER; SMOKE;

ASYMMETRIC VORTEX FLOWS; CIRCULAR CONES; EXPERIMENTAL INVESTIGATIONS; HIGH ANGLES OF ATTACK; LASER LIGHT PLANES; LOW SPEED; OSCILLATING MODES; VORTEX PAIR;

VORTEX FLOW;

EID: 84983138480     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-3389     Document Type: Conference Paper

References (3)

1. Stahl, W. H. and Asghar, A. "Dependancc on Reynolds Number of Onset of Vortex Asymmetry Behind Circular Cone," AIAA Paper 96-0064, Jan. 1996.
2. nd ed., Oxford University Press, Oxford, 1987, pp. 213-218, 327-329.
3. Lanford III, O. E., "The Strange Attractor Theory of Turbulence," Annual Review of Fluid Mechanics, Vol. 14, Annual Reviews Inc., Palo Alto, CA, 1982, pp. 347-364.