Mean flow of multistream rectangular jets under normal and mixing enhancement conditions

AIAA Paper

Volumn , Issue , 2004, Pages 11610-11630

  Papamoschou, Dimitri ^a   Dixon, Thomas T ^a   Nishi, Kimberley A ^a  

^a UNIVERSITY OF CALIFORNIA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL FLOW; JETS; NOZZLES; RESONANCE; REYNOLDS NUMBER; SUBSONIC AERODYNAMICS;

BYPASS RATIO; MULTISTREAM RECTANGULAR JETS; PARALLEL INJECTION;

AEROSPACE ENGINEERING;

EID: 2942746460     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-919     Document Type: Conference Paper

References (10)

1. [1] Papamoschou, D., "Mixing Enhancement Using Axial Flow," AIAA-2000-0093.
2. [2] Zaman, K.B.M.Q, and Papamoschou, D., "Study of Mixing Enhancement Observed with a Co-Annular Nozzle Configuration, " AIAA-2000-0094.
3. [3] Murakami, E. and Papamoschou, D., "Experiments on Mixing Enhancement in Dual-Stream Jets," AIAA-2001-0668.
4. [4] Zaman, K.B.M.Q, Wang, F.Y., and Georgiadis, N.J., "Noise, Turbulence, and Thrust of Sub-sonic Freejets from Lobed Nozzles," AIAA Journal, Vol. 41, No.3, 2003, pp. 398-407.
5. [5] Zaman KBMQ, Dahl MD, Bencic TJ, Loh CY, "Investigation of a "Transonic Resonance' with Convergent-Divergent Nozzles," Journal of Fluid Mechanics, Vol. 463, July 2002, pp. 313-343.
6. [6] Miller, E.H., and Migdal, D., "Separation and Stability Studies of a Convergent-Divergent Nozzle," AIAA Journal of Aircraft, Vol. 7, No.2, 1970, pp. 159-163.
7. [7] Wilmoth, R.G., and Leavitt, L.D., "Navier Stokes Predictions of Multifunction Nozzle Flows," Society of Automotive Engineers Transactions, Vol. 96, Sec.6, Paper 871753, 1987, pp. 6.865-6.879.
8. [8] Hunter, C.A., "Experimental, Theoretical and Computational Investigation of Separated Nozzle Flows," AIAA-98-3107.
9. [9] Zaman, K.B.M.Q., "Jet Spreading Increase by Passive Control and Associated Performance Penalty," AIAA-99-3505.
10. [10] Papamoschou, D. and Zill, A., "Supersonic Nozzle Flow Separation, " AIAA-2004-1111.