Experimental investigation of two-stream mixing flow with multiple tabs

AIAA Journal

Volumn 39, Issue 6, 2001, Pages 996-1005

  Yu, S C M ^a   Koh, P K ^a  

^a NANYANG TECHNOLOGICAL UNIVERSITY   (Singapore)

Author keywords

[No Author keywords available]

Indexed keywords

ANEMOMETERS; BOUNDARY LAYERS; LASER DOPPLER VELOCIMETERS; NAVIER STOKES EQUATIONS; PRESSURE; TURBULENCE; VELOCITY MEASUREMENT; VORTEX FLOW; VORTEX SHEDDING; WIND TUNNELS;

LASER DOPPLER ANEMOMETER; MULTIPLE TABS; SPLITTER PLATE; STREAMWISE VORTICES; TRAILING EDGE; TWO STREAM MIXING FLOW; VORTEX GENERATING TABS;

AIRCRAFT PARTS AND EQUIPMENT;

EID: 0035368243     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1428     Document Type: Article

References (17)

1. The distortion of a jet by tabs
2. The flow structure and statistics of a passive mixing tab
3. Heat transfer in counterswirled coaxial jet mixing
4. Experimental and numerical study of confined coaxial turbulent jets
5. Vortical and turbulent structure of a lobed forced mixer free-shear layer
6. Measurements of velocities in the near field of a lobed forced mixer trailing edge
7. Turbofan forced mixer lobe flow modeling vol. 1: Experimental and analytical assessment
8. Streamwise vorticity generation and mixing enhancement in free jets by 'delta-tabs'
9. Effect of tabs on the flow and noise field of an axisymmetric jet
10. Control of an axisymmetric jet using vortex generators
11. The evolution of a jet with vortex-generating tabs: Real time visualization and quantitative measurements
12. Near exit plane effects caused by primary and primary-plus-secondary tabs
13. Large and small scale vortical motions in a shear layer perturbed by tabs
14. A measurements of turbulence transport properties with a Laser-Doppler velocimeter
15. Experimental study of a three dimensional, shear driven turbulent boundary layer
16. Experimental studies of two-stream mixing flows with vortex-generating tabs