Mixing enhancement by tabs in round supersonic jets

4th AIAA/CEAS Aeroacoustics Conference

Volumn , Issue , 1998, Pages 731-746

  Seiner, John M ^a   Grosch, C E ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b OLD DOMINION UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROACOUSTICS; MASS TRANSFER; MIXING; NOZZLES; NUMERICAL MODELS; SHEAR FLOW; SUPERSONIC AERODYNAMICS; VORTICITY;

AXISYMMETRIC NOZZLES; COUNTER ROTATING; ENTRAINMENT RATES; EXPERIMENTAL TEST; MIXING ENHANCEMENT; MIXING PROCESS; SUPERSONIC JETS; VORTEX STRENGTH;

FIGHTER AIRCRAFT;

EID: 84977079464     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-2326     Document Type: Conference Paper

References (9)

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2. Drummond, J.P., Carpenter, M.H., Riggins, D.W., and Adams, M.S., “Mixing Enhancement in a Supersonic Combustor”, AIAA Paper No. 89-2794, 1989.
3. Ahuja, K.K., and Brown, W.H., “Shear Flow Control by Mechanical Tabs”, AIAA Paper No. 89-0994, 1989.
4. Samimy, M., Zaman, K.B.M.Q., and Reeder, M.F., “Effect of Tabs On The Flow and Noise Field of An Axisymmeric Jet”, AIAA 1,31,609(1993).
5. Zaman, K.B.M.Q., Reeder, M.F., and Samimy, M., “Control of an Axisymmetric Jet Using Vortex Generators”, Phys. Fluids, 6, 778, 1994.
6. Seiner, J.M., “Fluid Dynamics and Noise Emission Associated With Supersonic Jets”, Studies In Turbulence, Springer Verlag, pp 297-323, 1991
7. Peyret, R. and Taylor, T.D., “Computational Methods for Fluid Flow”, Springer-Verlag, New York Heidelberg Berlin, 1983.
8. Grinstein, F.F., Gutmark, E.J., Parr, T.P., Hanson-Parr, D.M., and Obeysekare, U., “Streamwise and Spanwise Vortex Interaction in an Axisymmetric Jet. A Computational and Experimental Study”, Physics of Fluids, 8, 1515 (1996).
9. Grosch, C.E., Seiner, J.M., Hussani, M.Y., and Jackson, T.L.,”Numerical Simulation of Mixing Enhancement in a Hot Supersonic Jet”, Phys. Fluids, 9, 1125, 1997.