Future directions in turbulence modeling for jet flowfield simulation

2nd AIAA/CEAS Aeroacoustics Conference

Volumn , Issue , 1996, Pages

  Dash, Sanford M ^a   Kenzakowski, Donald C ^a  

^a Syst Simulation Dvmt Directorate   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROACOUSTICS; FLOW FIELDS; LARGE EDDY SIMULATION; TURBULENCE MODELS;

ADAPTIVE EMBEDDING; COMPLEX FLOW STRUCTURES; FAST SCREENING; FLOW FIELD SIMULATION; MODEL DEVELOPMENT; MODELING CONCEPTS;

FIGHTER AIRCRAFT;

EID: 84977144647     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1775     Document Type: Conference Paper

References (24)

1. Khavaran, A., Krejsa, E.A., and Kim, C.M., “Computation of Supersonic Jet Mixing Noise for an Axisymmetric CD Nozzle,” J. Aircraft, Vol. 3, No. 31, 1994.
2. Viswanathan, D. and Sankar, L.N., “Toward the Direct Calculation of Noise: Fluid/Acoustic Coupled Simulation,” AIAA J., Vol. 33, No. 12,1995.
3. Mankabadi, R.R., Hixon, R., Shih, S.H., and Povinelli, L.A., “On the Use of Linearized Euler Equations in the Prediction of Jet Noise,” AIAA Paper No. 95-0505,January 1995.
4. Bangalore, A., Morris, P., and Long, L., “A Parallel Three-Dimensional Computational Aeroacoustics Method Using Non-Linear Disturbance Equations,” AIAA Paper 96-1728, 2nd AIAA/CEAS Aeroacoustics Conference, May 1996.
5. Sinha, N. and Dash, S.M., “Large Eddy Simulation of Supersonic Jets and Steps Towards Source Noise Prediction,” AIAA/CEAS-95-146, First Joint CEAS/AIAA Aeroacoustics Conf. (16th AIAA Aeroacoustics Conf.), Munich, Germany, June 1995.
6. Sinha, N., Lee, R.A., Dash, S.M., and Pelz, R.B., “Advances in 3D Unsteady Jet Simulation Using LES Methodology in a Parallel Environment,” AIAA-96- 1779, 2nd AIAA/CEAS Aeroacoustics Conf. (17th AIAA Aeroacoustics Conf.), May 6-8, 1996.
7. Lyrintzis, A.S. and Mankabadi, R.R., “On the Prediction of the Far-fields Jet Noise Using Kirchhoff's Formulation,” AIAA Paper No. 95-0508, Jan. 1995.
8. Dash, S.M. and Kenzakowski, D.C., “A Compressible-Dissipation Extension to the ke Turbulence Model and Building-Block Data for its Validation,” AIAA-92-2766, 1992 AIAA SDIO Technology Conference, May 19-21, 1992.
9. Dash, S.M., Kenzakowski, D.C. and Sinha, N., “Progress in the Development and Assessment of Improved Turbulence Models for Plume Flowfield Simulation,” 20th JANNAF Exhaust Plume Mtg., Phillips Lab., Kirtland AFB, NM, February 9-11,1993.
10. Dash, S.M., Kenzakowski, D.C., Seiner, J.M., and Bhat, T.R.S., “Recent Advances in Jet Flowfield Simulation: Part I - Steady Flows,” AIAA 93-4390, 15th AIAA Aeroacoustics Conf., Oct. 25-27, 1993.
11. Dash, S.M., Kenzakowski, D.C., Lee, R. A., and Sinha, N., “Simulation of Hot Laboratory Jets - Modeling Advances and Data Comparisons,” AIAA/CEAS-95-072, First Joint CEAS/AIAA Aeroacoustics Conf., June 12-15, 1995.
12. Speziale, C.G., Raj, R. and Gatski, T.B., “Modeling the Dissipation Rate in Rotating Turbulent Flows,” Studies in Turbulence. Springer-Verlag, 1991.
13. Heltsley, F.L. and Crosswy, F., “Investigation of Plume-Induced Separation on a Generic Zero-Based Missing Afterbody at Supersonic Speed,” AEDC-TR- 88-5, April 1989.
14. Kennedy, K.D., Walker, B.J., and Mikkelsen, C.D., “Missile Exhaust Plume Mixing Comparison,” presented at TTCP 21st WTP-2 Meeting, DSTO, Adelaide, South Australia, 29 April-3 May, 1996.
15. Petrie, H. and Walker, B.J., “Tactical Missile Base Flow Investigation,” 15th JANNAF Exhaust Plume Tech. Mtg., Ft. Sam Houston, TX, May 1985.
16. Childs, R.E. and Caruso, S.C., “Assessment of Modeling and Discretization Accuracy for High-Speed Afterbody Flows,” J. Propulsion, Vol. 7, No. 4,1991.
17. Gallardo, J-F and Lakshminarayana, B., “Computation of Curved Flows Using a Modified k-e Model of Turbulence Based on Algebraic Reynolds Stress Relations,” AIAA Paper No. 93-0202, Jan. 1993.
18. De, P., Robertson, D., Kenzakowski, D.C., and Dash, S.M., “C-17A Turbofan Exhaust Plumes Calculated with the EXTF/SPLITP Flowfield Model,” 4th JANNAF SPIRITS Users Group Mtg., October, 1995.
19. Dash, S.M., Sinha, N., York, B.J., Lee, R.A., and Hosangadi, A., “On the Inclusion of Advanced Turbulence Models and Nonequilibrium Thermochemistry into State-of-the-Art CFD Codes and Their Validation,” AIAA-92-2764, 1992.
20. Lee, R.A. and Dash, S.M., “Helicopter Exhaust Plume Flowfield Simulation for SPIRITS-HC,” presentation at EOATMUM92, Naval Air Warfare Center, Point Mugu, CA, Oct. 20-22, 1992.
21. Hosangadi, A., Lee, R.A., York, B.J., Sinha, N., and Dash, S.M., “A Three-Dimensional Unstructured Flow Solver for Reacting Multiphase Propulsive Flows,” AIAA-95-0258, January 9-12, 1995.
22. Dash, S.M., Sinha, N., York, B.J., Hosangadi, A., Lee, R.A., and Kenzakowski, D.C.., “Hybrid Structured/Unstructured Simulation of Multiphase Rocket Propulsive Flowfields,” AIAA-95-2780, 31st AIAA Joint Propulsion Conf., July 10-12,1995.
23. Lee, R.A., Hosangadi, A., N. Sinha, B.J. York, and Dash, S.M., “Combustion and Multiphase Extensions to Upwind Unstructured Numerics for Plume-Oriented Flowfield Simulation,” 22nd JANNAF Exhaust Plume Tech. Mtg., NASA/MSFC, October 23-27, 1995.
24. Hosangadi, A., Lee, R.A., York, B.J., Sinha, N. and Dash, S.M., “Upwind Unstructured Scheme for Three- Dimensional Combusting Flows,” Journal, of Propulsion and Power, Vol. 12, No. 2, 1996.