Study of delayed-detached eddy simulation with weakly nonlinear turbulence model

Journal of Aircraft

Volumn 43, Issue 5, 2006, Pages 1377-1385

  Xiao, Zhixiang ^a,b   Chen, Haixin ^a,b   Zhang, Yufei ^a,b   Huang, Jingbo ^a,b   Fu, Song ^a,b,c  

^a TSINGHUA UNIVERSITY   (China)

^b School of Aerospace Engineering   (China)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; COMPUTER SIMULATION; NAVIER STOKES EQUATIONS; PARALLEL PROCESSING SYSTEMS; REYNOLDS NUMBER; TURBULENCE;

EDDY SIMULATION; TRANSONIC SEPARATION; TURBULENCE MODEL; WING VORTEX BREAKDOWN;

AERODYNAMICS;

EID: 33750802489     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.20127     Document Type: Article

References (26)

1. Spalart, P. R., Jou, W.-H., Strelets, M., and Allmaras, S. R., "Comments on the Feasibility of LES for Wings, and on a Hybrid RANS/LES Approach," Advanced in DNS/LES, edited by C. Liu and Z. Liu, Greyden Press, Columbus, OH, Aug. 1997.
2. Spalart, P. R., and Allmaras, S. R., "A One-Equation Turbulence Model for Aerodynamic Flows," AIAA Paper 92-0439, Jan. 1992.
3. Strelets, M., "Detached Eddy Simulation of Massively Separated Flows," AIAA Paper 2001-0879, Jan. 2001.
4. Menter, F. R., "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications," AIAA Journal, Vol. 32, No. 8, 1994, pp. 1598-1605.
5. Davidson, L., "Hybrid LES-RANS: A Comparison of a One-Equation SGS Model and a k-l Model for Prediction Recirculation Flows," European Congress on Computational Methods in Applied Science and Engineering. Computational Dynamics Conference, 2001, ECCO-MAS, Swansea, Wales, U.K., Sept. 2001.
6. Baurle, R. A., Tam, C.-J., Edwards, J. R., and Hassan, H. A., "Hybrid Simulation Approach for Cavity Flows: Blending, Algorithm, and Boundary Treatment Issues," AIAA Journal, Vol. 41, No, 8, 2003. pp. 1463-1480.
7. Menter, F. R., and Kuntz, M., "A Zonal SST-DES Formulation," DES-WORKSHOP, July 2003 (http://crd.me.umist.ac.uk/flomania/index2.html).
8. Simon, F., Deck, S., Guillen, P., and Sagaut, P., "Hybrid RANS-LES Simulations of Supersonic Base Flow," Symposium on Hybrid RANS/LES Methods, FOI, edited by S.-H. Peng and W. Haase, 2005.
9. Squires, K. D., Forsythe, J. R., Morton, S. A., Strang, W. Z., Wurtzler. K. E., Tomaro, R. F., Grismer, M. J., and Spalart, P. R., "Progress on Detached-Eddy Simulation of Massively Separated Flows," AIAA Paper 2002-1021, Jan. 2002.
10. Forsythe, J. R., Hoffmann, K. A., Cummings, R. M., and Squires, K. D., "Detached-Eddy Simulation With Compressibility Corrections Applied to a Supersonic Axisymmetric Base Flow," Journal of Fluids Engineering, Vol. 124, No. 4, Dec. 2002, pp. 911-923.
11. Viswanathan, A. K., Klismith, K. R., Forsythe, J. R., and Squires, K. D., "Detached-Eddy Simulation Around a Forebody at High Angle of Attack," AIAA Paper 2003-0263, Jan. 2003.
12. Kotapati-Apparao, R. B., Squires, K. D., and Forsythe, J. R., "Prediction of the Flow over an Airfoil at Maximum Lift," AIAA Paper 2004-0259, Jan. 2004.
13. Krishnan, V., Squires, K. D., and Forsythe, J. R., "Prediction of Separated Flow Characteristics over a Hump Using RANS and DES," AIAA Paper 2004-2224, July 2004.
14. Constantinescu, G., and Squires, K. D., "Numerical Investigations of Flow over a Sphere in the Sub-Critical and Supercritical Regimes," Physics of Fluids, Vol. 16, No. 5, 2004, pp. 1449-1466.
15. Wilcox, D. C., "Reassessment of the Scale-Determining Equation for Advanced Turbulence Models," AIAA Journal, Vol. 26, No. 11, 1988, pp. 1299-1310.
16. Fu, S., Rung, T., and Thiele, F., "Realizability of the Nonlinear Stress-Strain Relationships for Reynolds-Stress Closure," Proceedings of the 11th Symposium on Turbulent Shear Flows, Sep. 1997.
17. Soo, H.-P., and Jang, H.-K., "Implementation of k-ω Turbulence Models in an Implicit Multigrid Method," AIAA Journal, Vol. 42, No. 7, 2004, pp. 1348-1357.
18. Durbin, P. A., "On the k-ε Stagnation Point Anomaly," International Journal of Heat and Fluid Flow, Vol. 17, No. 1, 1996, pp. 89-90.
19. Xiao, Z.-X., Chen, H.-X., Fu, S., and Li, F.-W., "Computations with k-g Model for Complex Configurations at High-Incidence," Journal of Aircraft, Vol. 42, No. 2, 2005, pp. 462-468.
20. 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.
21. Roe, P. L., "Approximate Riemann Solver, Parameter Vectors, and Difference Schemes," Journal of Computational Physics, Vol. 43, No. 2, 1981, pp. 357-372.
22. Radespiel, R., and Swanson, R. C., "Progress with Multi-Grid Schemes for Hypersonic Flow Problems," NASA TR CR 189579, 1991.
23. Li, J., Li, F.-W., and E, Q., "A Fully Implicit Method for Steady and Unsteady Viscous Flow Simulations," Journal for Numerical Methods in Fluids, Vol. 43, No. 2, 2003, pp. 147-163.
24. Smagorinsky, J., "General Circulation Experiments with Primitive Equations. I. The Basic Experiment," Monthly Weather Review, Vol. 91, No. 3, 1963, pp. 99-164.
25. 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.
26. Yoon, S., and Jameson, A., "Lower-Upper Symmetric-Gauss-Seidel Method for the Euler and Navier-Stokes Equations," AIAA Paper 87-0600, Jan. 1987.