Role of turbulent Prandtl number on heat flux at hypersonic mach numbers

43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers

Volumn , Issue , 2005, Pages 10119-10131

  Xiao, X ^a,c,d   Edwards, J R ^a,c,d   Hassan, H A ^a,c,d   Gaffney Jr , R L ^b,d,e  

^a NORTH CAROLINA STATE UNIVERSITY   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Dept of Mechanical and Aerospace Engineering ^*  (United States)

^d AIAA   (United States)

^e Hypersonic Air Breathing Propulsion Branch

Author keywords

[No Author keywords available]

Indexed keywords

ENTHALPY; HEAT FLUX; HYPERSONIC AERODYNAMICS; MATHEMATICAL MODELS; PRANDTL NUMBER; TRANSFER FUNCTIONS;

DISSIPATION RATES; MACH NUMBER; TURBULENCE MODEL;

TURBULENCE;

EID: 30744472182     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-1098     Document Type: Conference Paper

References (11)

1. Thivet, F., Knight, D. D., Zheltovodov, A. A., and Maksimov, A. I., "Insights in Turbulence Modeling for Crossing-Shock Wave/Boundary-Layer Interactions," AIAA Journal, Vol. 39, No. 6, 2001, pp. 985-995.
2. Morkovin, M., "Effects of Compressibility on Turbulent Flows," Mecanique de le Turbulence, edited by A. Favre, Gordon and Breach, New York, 1964, pp. 367-380.
3. Sommer, T. P., So, R. M. C., and Zhang, H. A., "Near-Wall Variable-Prandtl-Number Turbulence Model for Compressible Flows," AIAA Journal, Vol. 31, No. 1, 1993, pp. 27-35.
4. Abe, K., Kondoh, T., and Nagano, Y., "A New Turbulence Model for Predicting Flow and Heat Transfer in Separating and Reattaching Flows - II. Thermal Field Calculations," International Journal of Heat and Mass Transfer, Vol. 38, No. 4, 1995, pp. 1467-1481.
5. Robinson, D. F. and Hassan, H. A., "Further Development of the k-ζ (Enstrophy) Turbulence Closure Model," AIAA Journal, Vol. 36, No. 10, 1998, pp. 1825-1833.
6. Coleman, G. G. and Stollery, J. L., "Heat Transfer from Hypersonic Turbulent Flow at a Wedge Compression Corner," Journal of Fluid Mechanics, Vol. 56, No. 4, 1972, pp. 741-752.
7. Kussoy, M. I., Horstman, K. C., and Horstman, C. C., "Hypersonic Crossing Shock-Wave/Turbulent Boundary Interactions," AIAA Journal, Vol. 31, No. 12, 1993, pp. 2197-2203.
8. Kimmel, R. L., Poggie, J., and Schwoerke, S. N., "Laminar-Turbulent Transition in a Mach 8 Elliptic Cone Flow," AIAA Journal, Vol. 37, No. 9, 1999, pp. 1080-1087.
9. Schülein, E., "Optical Skin Friction Measurements in Short-Duration Facilities," AIAA Paper 2004-2115, June 2004.
10. Schülein, E., Krogmann, P., and Stanwsky, E., "Documentation of Two-Dimensional Impinging Shock/Turbulent Boundary Layer Interaction Flows," DLR l B 223-96 A 49, October 1996.
11. Nance, R. P. and Hassan, H. A., "Turbulence Modeling of Shock-Dominated Flow with a k-ζ, Formulation," AIAA Paper 99-0153, January 1999.