Assessment of turbulence-chemistry interactions in missile exhaust plume signature analysis

Journal of Spacecraft and Rockets

Volumn 40, Issue 5, 2003, Pages 694-695

  Calhoon Jr , W H ^a   Kenzakowski, D C ^a  

^a Syst Simulation Dvmt Directorate   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; EXHAUST SYSTEMS (ENGINE); MATHEMATICAL MODELS; PROBABILITY DENSITY FUNCTION; REYNOLDS NUMBER; STATISTICAL METHODS; TURBULENCE;

PLUME SIGNATURE; SOFTWARE PACKAGE CRAFT CFD; TURBULENCE-CHEMISTRY INTERACTIONS;

MISSILES;

EID: 0142149028     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.6895     Document Type: Article

References (8)

1. Dash, S. M., Pearce, B. E., Pergament, H. S., and Fishburne, E. S., "Predictions of Rocket Plume Flowfields for Infrared Signature Studies," Journal of Spacecraft and Rockets, Vol. 17, No. 3, 1980, pp. 190-199.
2. Calhoon, W. H., Jr., "Computational Assessment of Afterburning Cessation Mechanisms in Fuel Rich Rocket Exhaust Plumes," Journal of Propulsion and Power, Vol. 17, No. 1, 2001, pp. 111-119.
3. Gaffney, R. L., Jr., White, J. A., Girimaji, S. S., and Drummond, J. P., "Modeling Turbulent/Chemistry Interactions Using Assumed PDF Methods," AIAA Paper 92-3638, July 1992.
4. Gaffney, R. L., Jr., White, J. A., Girimaji, S. S., and Drummond, J. P., "Modeling Turbulent and Species Fluctuations in Turbulent, Reacting Flow," Computing Systems in Engineering, Vol. 5, No. 2, 1994, pp. 117-133.
5. Hsu, A. T., Tsai, Y.-L. P., and Raju, M. S., "Probability Density Function Approach for Compressible Turbulent Reacting Flows," AIAA Journal, Vol. 32, No. 7, 1994, pp. 1407-1415.
6. Delarue, B. J., and Pope, S. B., "Calculation of Subsonic and Supersonic Turbulent Reacting Mixing Layers Using Probability Density Function Methods," Physics of Fluids, Vol. 10, No. 2, 1998, pp. 487-498.
7. Calhoon, W. H., Jr., and Kenzakowski, D. C., "Flowfield and Radiation Analysis of Missile Exhaust Plumes Using a Turbulent-Chemistry Interaction Model," AIAA Paper 2000-3388, July 2000.
8. Sinha, N., Dash, S. M., and Hosangadi, A., "Applications of an Implicit, Upwind NS Code, CRAFT, to Steady/Unsteady Reacting, Multi-Phase Jet/Plume Flowfields," AIAA Paper 92-0837, Jan. 1992.