Investigation of supersonic jet exhaust flow by one- and two-equation turbulence models

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Suzen, Yildirim B ^a   Hoffinann, Klaus A ^a  

^a Wichita State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; FLOW FIELDS; FLOW MEASUREMENT; SHOCK WAVES; SUPERSONIC AERODYNAMICS; TURBULENCE MODELS;

COMPRESSIBILITY CORRECTION; FLOW FIELD SIMULATION; FLUX VECTOR SPLITTING SCHEMES; LOGICAL APPROACHES; ONE-EQUATION MODEL; SUPERSONIC JET FLOW; TWO-EQUATION MODEL; TWO-EQUATION TURBULENCE MODELS;

SHEAR FLOW;

EID: 84983191340     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-322     Document Type: Conference Paper

References (30)

1. Marvin, J. G., "Turbulence Modeling for Computational Aerodynamics," AIAA-82-0164, 1982.
2. Bushnell, D. M, "Turbulence Modeling in Aerodynamic Shear Flow-Status and Problems," AIAA-91-0214, January 1991.
3. Patel, V. C., Rodi, W., and Scheuerer, G., "Turbulence Models for Near-Wall and Low Reynolds Number Flows: A Review" AIAA Journal, Vol. 23, No. 9, pp. 1308-1319, 1985.
4. Baldwin, B., Barth, T. J., "A One-Equation Turbulence Transport Model for High Reynolds Number Wall-Bounded Flows," NASA-TM-102847, August 1990.
5. Spalart, P. R. and Allmaras, S. R., "A One-Equation Turbulence Model for Aerodynamic Flows," AIAA-92-0439, January 1992.
6. Menter, F. R., "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications," ALAA Journal, Vol. 32, No. 8, August 1994, pp. 1598-1605.
7. Nash, K., Whitaker, K., and Freeman, L. M., "A Simplified Exhaust Plume Prediction Method for Underexpanded Nozzles in Supersonic Exhaust Flows," AIAA-91-2371, June 1991.
8. VonGlahn, U. N., "Rectangular Nozzle Plume Velocity Modeling for Use in Jet Noise Prediction," N89-22577.
9. Ajdari, E., Gutmark, E., Parr, T. P., Wilson, K. J., and Schadow, K. C., "Thermal Imaging of Afterburning Plumes," AIAA-89-0062, Januarty 1989.
10. Scallion, W. I., "Effects of Nozzle Exit Geometry and Pressure Ratio on Plume Shape for Nozzles Exhausting into Quiescent Air," N91-24129.
11. Heinemann, K., and Keener, E. R., "Experimental Research of the Aerodynmaics of Nozzles and Plumes at Hypersonic Speeds," NCC2-553, January 1992, N92-15048.
12. Chiang, S. T., Hoffinann, K. A., and Wilson, D. E., "Near Field Computation of Rocket Exhaust Flow," AIAA-91-0710, Januaiy 1991.
13. Tassa, Y., Gogineni, P., and Kirch, H., "Rocket Exhaust Plume/Air Interaction at High Altitude Via Navier-Stokes Solver," AIAA-89-1767, January 1989.
14. Hsu, A. T., and Liou, M. S., "Computational Analysis of Underexpanded Jets in the Hypersonic Regime," Journal of Propulsion, Vol. 7, No. 2, March-April 1991, pp., 297-299.
15. Feiereisen, W. J., and Venkatapathy E., "Computations of Ideal and Real Gas High Altitude Plume Flows," AIAA-88-2636, June 1988.
16. Venkatapathy, E., and Feiereisen, W. J., "Computational Analysis of Plume Induced Separation," AIAA-91-0711, January 1991.
17. Slotnick, J. P., Kandula, M., Buning, P. G., and Martin, F. W., "Numerical Simulation of the Space Shuttle Launch Vehicle Flowfield with Real Gas Solid Rocket Motor Plume Effects," AIAA-93-0521, January 1993.
18. 2 Rocket Engine Plume Flow Studies," AIAA-91-0246, January 1991.
19. Holcomb, J. E., "Three Dimensional Navier-Stokes Rocket Plume Calculations," AIAA-89-1986CP, June 1989.
20. Childs, R. E., Caruso, S. C., "Assessment of Modeling and Discretization Accuracy for high-Speed Afterbody Flows," Journal of Propulsion, Vol. 7, No. 4, August 1991, pp. 607-616.
21. Viegas, J. R., Rubesin, M W., "Assesssment of Compressibility Corrections to the k-ε Model in High Speed Shear Layers," AIAA Journal, Vol. 30, No. 10, October 1992, pp. 2369-2370.
22. Dash, S. M., Kenzakowski, D. C., "A Compressible Dissipation Extension of the k-ε Turbulence Model and Building-Block Data for its Validation," AIAA-92-2766, May 1992.
23. Lakshmanan, B., Abdol-Hamid, K. S., "Investigation of Supersonic Jet Plumes Using an Improved Two-Equation Turbulence Model," Journal of Propulsion and Power, Vol. 10, No. 5, Sept-Oct. 1994, pp. 736-741.
24. Balakrishnan, L., and Abdol-Hamid, K. S., "A Comparitive Study of Two Codes with an Improved Two-Equation Turbulence Model for Predicting Jet Plumes," AIAA-92-2604-CP, 1992.
25. Dash, S. M., "Observations on Practical Turbulence Modeling for High-Speed Jet/Plume Flowfields," AIAA-91-1789, June 1991.
26. Seiner, J. M., and Norum, T. D., "Experiments of Shock Associated Noise on Supersonic Jets," AIAA-79-1526, AIAA 12th Fluid and Plasma Dynamics Conference, July 1979.
27. Steger, J. L., and Warming, R. F., "Flux Vector Splitting of the Inviscid Gasdynamic Equations with Application to Finite Difference Methods," NASA TM-78605, June 1979.
28. Wilcox, D. C., "Reassessment of the Scale-Determining Equation for Advanced Turbulence Models," AIAA Journal, Vol. 26, Nov. 1988, pp. 1299-1310.
29. Menter, F. R., "Zonal Two Equation k-ω Turbulence Models for Aerodynamic Flows," AIAA-93-2906, July 1993, Orlando, Florida.
30. Menter, F. R., Rumsey, C. L., "Assessment of Two-Equation Turbulence Models for Transonic Flows," AIAA-94-2343, June 1994.