Prediction of hypersonic shock wave turbulent boundary layer interactions with the k-l two equation turbulence model

33rd Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1995, Pages

  Smith, Brian R ^a,b  

^a Lockheed Fort Worth Company   (United States)

^b CFD Group   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; HEAT TRANSFER; HYPERSONIC BOUNDARY LAYERS; SHOCK WAVES; TURBULENCE MODELS;

COMPRESSIBILITY CORRECTION; HEAT TRANSFER DATA; LENGTH SCALE EQUATIONS; NAVIER-STOKES SOLVER; SURFACE PRESSURES; TURBULENT BOUNDARY LAYERS; TURBULENT BOUNDARY-LAYER INTERACTIONS; TWO-EQUATION TURBULENCE MODELS;

NAVIER STOKES EQUATIONS;

EID: 0040238395     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

1. Smith, B. R., A Near Wall Model for the k - I Two Equation Turbulence Model, AIAA Paper 94-2386.
2. Huang, P. G. and Coleman, G. N. “Van Driest Transformation and Compressible Wall-Bounded Flows,” AIAA Journal, Vol 32, no. 10, Oct. 1994, pp. 2110-13.
3. Huang, P. G., Bradshaw, P. and Coakley, T. J., “Turbulence Models for Compressible Boundary Layers”, AIAA Journal, Vol 32, No. 4, Apr. 1994, pp. 73540.
4. Kussoy, M. I. and Horstman, K. C, “Documentation of Two- and Three-Dimensional Shock-Wave/Tur-butentrBoundary-Layer Interaction Flows at Mach 8.2,” NASA TM 103838, May, 1991.
5. Kussoy, M. I. and Horstman, K. C, Intersecting Shock-Wave/Turbulent Boundary-Layer Interactions at Mach 8.3, NASA TM 103909, Feb. 1992.
6. Kussoy, M. I., and Horstman, K. C, and Horstman, C. C. “Hypersonic Crossing Shock-Wave/Turbulent-Boundary-Layer Interactions,” AIAA Journal, Vol. 31, No. 12, December 1993, pp. 2197-2203.
7. Horstmann, C. C, “Hypersonic Shock-Wave Turbulent Boundary Layer Interaction Flows-Experiment and Computation,” AIAA Paper 91-1790.
8. Narayanswami, N., Horstman, C.C., and Knight, D. D. “Computation of Crossing Shock/Turbulent Boundary Layer Interaction at Mach 8.3”, AIAA Journal, Vol. 31, No. 8, August 1993, pp. 1369-76
9. Bardina, J. E. and Coakley, T. J, Three-Dimensional Navier-Stokes Simulations with Two-Equation Turbulence Models of Intersecting Shock-Wave/Turbulent boundary Layer at Mach 8.3, AIAA Paper 94-1905.
10. Roe, P. L., “Characteristic-Based Schemes for the Euler Equations,” Annual Review of Fluid Mechanics, Vol. 18, 1986, pp. 337-365.
11. Van Leer, B., Lee, W., and Powell, K. G., “Sonic-Point Capturing,” AIAA Paper 89-1945-CP.
12. Smith, B. R. “The k - kl turbulence Model and Wall Layer Model for Compressible Flows,” AIAA Paper 90-1483.
13. Coakley, T. J., Horstman, C. C, Marvin, J. G., Viegas, J. R., Bardina, J. E., Huang, P. G., and Kussoy, M. I., “Turbulence Compressibility Corrections,” NASA TM 108827, May 1994.