Jet mixing enhancement using fluid tabs

2nd AIAA Flow Control Conference

Volumn , Issue , 2004, Pages

  Behrouzi, Parviz ^a   Mcguirk, James J ^a  

^a LOUGHBOROUGH UNIVERSITY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AXISYMMETRIC NOZZLES; JET FLOW RATE; JET MIXING ENHANCEMENT; LENGTH REDUCTION; NOZZLE EXITS; STREAMWISE VORTICES; VELOCITY DECAY; WATER TUNNEL;

DECAY (ORGANIC); FLOW CONTROL; NOZZLES;

MIXING;

EID: 84897769491     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

1. Seiner J. M., Dash S. M., and Kenzakowski D.C., "Historical survey on enhanced mixing in scramjet engines," AIAA Jnl.of Propulsion and Power, Vol 17, pp 1273-1286, 2001.
2. Bradbury L.J.S. and Khadem A.H., "The distortion of a jet by tabs," Jnl. of Fluid Mechanics, Vol. 70, pp 801-813, 1975.
3. Bohl D.G. and Foss J.F., "Streamwise vorticity and velocity measurements in the near-field of a tabbed jet", Conference on Turbulence in Complex Flows, ASME Fluids Engineering Division, Vol 203, 1994.
4. Bohl D.G. and Foss J.F., "Near exit plane effects caused by primary and primary-plus-secondary tabs," AIAA Jnl., Vol. 37, pp 192-201, 1999.
5. Samimy M., Zaman K.B.M.Q., and Reeder M.F., "Effect of tabs on the flow and noise field of an axisymmetric jet," AIAA Jnl., Vol. 31, pp 609-615, 1993.
6. Zaman K.B.M.Q., Reeder M.F., and Samimy M., "Supersonic jet mixing enhancement by delta-tabs," AIAA 92-3548, 1992.
7. Reeder M.F. and Samimy M., "The evolution of a jet with vortex-generating tabs: real-time visualisation and quantitative measurements," Jnl. of Fluid Mechanics, Vol 311, pp 73-118, 1996.
8. Behrouzi P. and McGuirk J.J., "Experimental studies of tab geometry effects on mixing enhancement of an axisymmetric jet," JSME International Journal, Series B, Vol. 41, pp 908-917, 1998.
9. Bohl D.G. and Foss J.F., "Enhancement of passive mixing tabs by the addition of secondary tabs," AIAA 96-0545, 1996.
10. th AIAA-CEAS Aeroacoustics Conference, AIAA Paper 2000-1961, 2000.
11. Reddy D.R., Steffen C.J., and Zaman K.B.M.Q., "Computation of 3D compressible flow from a rectangular nozzle with delta tabs," ASME Paper 97-GT-257, 1997.
12. th AIAA-CEAS Aeroacoustics Conference, AIAA Paper 2003-3286, 2003.
13. th AIAA-CEAS Aeroacoustics Conference, AIAA Paper 2003-3287, 2003.
14. Bray T.P. and Garry K.P., "Optimisation of air jet vortex generators with respect to system design parameters," The Aeronautical Journal, Vol. 103, pp 475-480, 1999.
15. Suzuki T., Nagata M., Shizawa T., and Honami S., "Optimal injection condition of a single pulsed vortex generator jet to promote cross-stream mixing," Experimental Thermal and Fluid Science, Vol. 17, pp 139-146, 1998.
16. th Int. Symp. on Air Breathing Engines, Vol. 1, pp 864-875, 1991.