Computations with k-g model for complex configurations at high-incidence

Journal of Aircraft

Volumn 42, Issue 2, 2005, Pages 462-468

  Xiao, Zhixiang ^a   Chen, Haixin ^a   Fu, Song ^a   Li, Fengwei ^b,c  

^a TSINGHUA UNIVERSITY   (China)

^b NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

^c North West Polytechnology University   (China)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MODELS; BOUNDARY CONDITIONS; COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL METHODS; COMPUTER SIMULATION; MATHEMATICAL MODELS; REYNOLDS NUMBER; TRANSONIC FLOW; WINGS;

EDDY VISCOSITY; SHEAR STRESS TRANSPORT (SST); TURBULENCE MODELS; WING JUNCTIONS;

TURBULENCE;

EID: 18144369321     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.6821     Document Type: Article

References (15)

1. Kandula, M., and Wilcox, D. C., "An Examination of k-ω Turbulence Model for Boundary Layers, Free Shear Layers and Separated Flows," AIAA Paper 95-2317, June 1995.
2. Wilcox, D. C., "Reassessment of the Scale-Determining Equation for Advanced Turbulence Models," AIM Journal, Vol. 26, No. 11, 1988, pp. 1299-1310.
3. Menter, F. R., "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications," AIAA Journal, Vol. 32, No. 8, 1994, pp. 1598-1605.
4. Kalitzin, G., Gould, A. R. B., and Benton, J. J., "Application of Two-Equation Turbulence Models in Aircraft Design," AIAA Paper 96-0327, Jan. 1996.
5. Runckel, J. F., and Lee, E. E., Jr., "Investigation at Transonic Speeds of the Loading over a 45 deg Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and NACA 65A004 Airfoil Sections," NASA TN D-712, May 1961.
6. Fengwei, L., Qin, E., Jie, L., Guowei, Y., and Haixin, C., "The Strategy on Grids Generation for Real Aircraft and Application in CFD for Aviation," First Numeric Grids Generation Methods Conference, Aug. 1997.
7. Bladwin, B., and Lomax, H., "Thin-Layer Approximation and Algebraic Model for Separation Flows," AIAA Paper 78-257, Jan. 1978.
8. Wilcox, D. C., Turbulence Modeling for CFD, 2nd edition, DCW Industries, Inc., La Canada, CA, 1998, Chap. 4.
9. Menter, F. R., "Zonal Two Equation k-ω Turbulence Models for Aerodynamic Flows," AIAA Paper 93-2906, July 1993.
10. Johnson, D. A., and King, L. S., "A Mathematical Simple Turbulence Closure Model for Attached and Separated Turbulent Boundary Layers," AIAA Journal, Vol. 23, No. 11, 1985, pp. 1684-1692.
11. Jameson, A., Schmidt, W., and Turkel, E., "Numerical Solutions of Euler Equations by Finite Volume Methods with Runge-Kutta Time Stepping Schemes," AIAA Paper 81-1259, June 1981.
12. Swanson, R. C., and Turkel, E., "Artificial Dissipation and Central Difference Schemes for Euler and N-S Equations," AIAA Paper 87-1107, June 1987.
13. Swanson, R. C., and Turkel, E., "On Central-Difference and Upwind Schemes," Journal of Computational Physics, Vol. 101, No. 2, 1992, pp. 292-306.
14. Couaillier, V, "Numerical Simulation of Separated Turbulent Flows Based on the Solution of RANS/Low Reynolds Two-Equation Model," AIAA Paper 99-0154, Jan. 1999.
15. Zhixiang, X., Jie, L., Fengwei, L., and Chuanjing, L., "Application of Turbulence Models in Simulation of Complex Flow-Fields," AIAA Paper 2003-3745, June 2003.