A zonal RANS-LES method for compressible flows

Computers and Fluids

Volumn 67, Issue , 2012, Pages 1-15

  Roidl, B ^a   Meinke, M ^a   Schroder W ^a  

^a RWTH AACHEN UNIVERSITY   (Germany)

Author keywords

Compressible turbulence; Shock wave boundary layer interaction; Zonal RANS LES method

Indexed keywords

COMPRESSIBLE TURBULENCE; CONTROL PLANES; FLOW PROBLEMS; LOW FREQUENCY PRESSURE; MEAN FLOW; NUMERICAL SCHEME; REFERENCE DATA; REYNOLDS STRESS DISTRIBUTION; REYNOLDS-AVERAGED NAVIER-STOKES; SHOCK-WAVE/BOUNDARY-LAYER INTERACTION; SMOOTH TRANSITIONS; TRANSITION LENGTH; TURBULENT BOUNDARY-LAYER INTERACTIONS; TURBULENT EDDY; WALL-SHEAR STRESS; ZONAL METHOD; ZONAL RANS-LES METHOD;

BOUNDARY LAYER FLOW; BOUNDARY LAYERS; COMPRESSIBLE FLOW; INTERNET PROTOCOLS; STRESS CONCENTRATION; TURBULENT FLOW;

NAVIER STOKES EQUATIONS;

EID: 84864487813     PISSN: 00457930     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compfluid.2012.07.003     Document Type: Article

References (55)

1. Adams N.A. Direct numerical simulation of turbulent compression corner flow. J Fluid Mech 2000, 420:47-83.
2. Alkishriwi N., Schröder W., Meinke M. A large-eddy simulation method for low Mach number flows using preconditioning and multigrid. Comput Fluids 2006, 35(10):1126-1136.
3. Batten P., Goldberg U., Chakravarthy S. Interfacing statistical turbulence closures with large-eddy simulation. AIAA J 2004, 42(3):485-492.
4. Bookey PB, Wyckham C, Smits AJ. Experimental investigations of Mach 3 shock-wave turbulent boundary layer interactions. AIAA Paper 2005-4899; 2005.
5. Boris J.P., Grinstein F.F., Oran E.S., Kolbe R.L. New insights into large eddy simulation. Fluid Dynam Res 1992, 10:199-228.
6. Bradshaw P., Ferriss D.H., Atwell N.P. Calculation of boundary layer development using the turbulent energy equation. J Fluid Mech 1967, 23:31-64.
7. Casey M, Wintergerste T. Best practice guidelines. ERCOFTAC; 2000.
8. Choi J.I., Edwards J.R., Baurle R.A. Compressible boundary-layer predictions at high Reynolds number using hybrid LES/RANS methods. AIAA J 2009, 47(9):2179-2193.
9. de Prisco G., Piomelli U., Keating A. Improved turbulence generation techniques for hybrid RANS/LES calculations. J Turbul 2008, 9(5):1-20.
10. Deck S. Zonal-detached-eddy simulation of the flow around a high-lift configuration. AIAA J 2005, 43:2372-2384.
11. Délery J, Marvin JG. Shock-wave boundary layer interactions. AGARD AGARDograph No. 280, Neuilly-sur-Seine, France; 1986.
12. di Mare L., Klein M., Jones W.P., Janicka J. Synthetic turbulence inflow conditions for large-eddy simulation. Phys Fluids 2006, 18(025107).
13. El-Askary W, Schröder W, Meinke M. LES of compressible wall-bounded flows. AIAA Paper (2003-3554); 2003.
14. Eléna M., Lacharme J.P. Turbulent boundary layer using a laser Doppler anemometer. J Mec Theor Appl 1988, 7(2):175-190.
15. Fares E., Schröder W. A general one-equation turbulence model for free shear and wall-bounded flows. Flow Turbul Combust 2004, 73:187-215.
16. Fröhlich J., Terzi D.v. Hybrid LES/RANS methods for the simulation of turbulent flows. Prog Aerosp Sci 2008, 44:349-377.
17. Garnier E., Sagaut P., Deville M. Large eddy simulation of shock/boundary-layer interaction. AIAA J 2002, 40(10):79-107.
18. Hellsten A., Wallin S. Explicit algebraic Reynolds stress and non-linear eddy-viscosity models. Int J Comput Fluid Dynam 2009, 23(4):349-361.
19. Jarrin N., Benhamadouche S., Laurence D., Prosser R. A synthetic-eddy-method for generating inflow conditions for large-eddy simulations. Int J Heat Fluid Flow 2006, 27:585-593.
20. Jeong J., Hussain F. On the identification of a vortex. J Fluid Mech 1995, 285:69-94.
21. Keating A., de Prisco G., Piomelli U. Interface conditions for hybrid RANS/LES calculation. Int J Heat Fluid Flow 2006, 27:777-788.
22. Klein M., Sadkiki A., Janicka J. A digital filter based generation of inflow data for spatially developing direct numerical or large eddy simulations. J Comput Phys 2003, 186(652).
23. Knight D.D., Yan H., Panaras A.G., Zheltovodov A.A. Advances in CFD prediction of shock wave turbulent boundary layer interactions. Prog Aerosp Sci 2003, 39:121-184.
24. König D., Schröder W., Meinke M. Embedded LES-to-RANS boundary in zonal simulations. J Turbul 2010, 11(7):1-25.
25. Kraichnan R.H. Inertial ranges in two-dimensional turbulence. Phys Fluids 1967, 10(7):1417-1423.
26. Lee B.H.K. Self-sustained shock oscillations on airfoils at transonic speeds. Prog Aerosp Sci 2001, 37:147-196.
27. Leschziner M., Drikakis D. Turbulence modelling and turbulent-flow computation in aeronautics. Aeronaut J 2002, 106(1061):349-383.
28. Liou M.-S., Steffen C.J. A new flux splitting scheme. J Comput Phys 1993, 107:23-39.
29. Loginov M.S., Adams N.A., Zheltovodov A.A. Large-eddy simulation of shock-wave/turbulent-boundary-layer interaction. J Fluid Mech 2006, 565:135-169.
30. Marusic I. On the role of large-scale structures in wall turbulence. Phys Fluids 2001, 13(735).
31. Meinke M., Schröder W., Krause E., Rister T. A comparison of second- and sixth-order methods for large-eddy simulations. Comput Fluids 2002, 31:695-718.
32. Pamiès M., Weiss P.-é., Garnier E., Deck S., Sagaut P. Generation of synthetic turbulent inflow data for large eddy simulation of spatially evolving wall-bounded flows. Phys Fluids 2009, 16(045103).
33. Piponniau S., Dussauge J.-P., Debiève J.F., Dupont P. A simple model for low-frequency unsteadiness in shock-induced separation. J Fluid Mech 2009, 629:87-108.
34. Pirozzoli S., Bernardini M. Direct numerical simulation database for impinging shock wave/turbulent boundary-layer interaction. AIAA J 2011, 49(6):1307-1312.
35. Pirozzoli S., Bernardini M. Turbulence in supersonic boundary layers at moderate Reynolds number. J Fluid Mech 2011, 10.1017/jfm.2011.368.
36. Pirozzoli S., Grasso F. Direct numerical simulation of impinging shock wave/turbulent boundary layer interaction at M=2.25. Phys Fluids 2006, 18(065113).
37. Pirozzoli S., Grasso F., Gatski T.B. Direct numerical simulation and analysis of spatially evolving supersonic turbulent boundary layer at M=2.25. Phys Fluids 2004, 16(3):530-545.
38. Pope S.B. Turbulent flows 2000, Cambridge University Press.
39. Priebe S., Wu M., Martín M.P. Direct numerical simulation of a reflected-shock-wave/turbulent-boundary-layer interactions. AIAA J 2009, 47(5):1173-1185.
40. Richez F., Mary I., Gleize V., Basdevant C. Zonal RANS/LES coupling simulation of a transitional and separated flow around an airfoil near stall. Theor Comput Fluid Dyn 2008, 22:305-315.
41. Schlüter JU. Consistent boundary conditions for integrated RANS/LES/simulations: LES inflow conditions. AIAA Paper (2003-3971); 2003.
42. Smirnov A., Shi S., Celik I. Random flow generation technique for large eddy simulations and particle dynamics modeling. J Fluids Eng 2001, 123:359-371.
43. Smits A.J., Dussauge J.P. Turbulent shear layers in supersonic flow 2006, Springer Verlag, New York. 2nd ed.
44. Spalart P.R. Strategies for turbulence modelling and simulations. Int J Heat Fluid Flow 2000, 21:252-263.
45. Spalart P.R., Jou W.H., Strelets M., Allmaras S.R. Comments on the feasibility of LES for wings, and on a hybrid RANS/LES approach. Advances on DNS/LES 1997, Greyden Press, Columbus, OH, pp. 137-147.
46. Spille A, Kaltenbach HJ. Generation of turbulent inflow data with a prescribed shear-stress profile. In: Third AFSOR conference on DNS and LES; 2001.
47. Terracol M., Manoha E., Herrero C., Labourrasse E., Redonnet S., Sagaut P. Hybrid methods for airframe noise numerical prediction. Theor Comput Fluid Dyn 2005, 19:197-227.
48. Touber E., Sandham N.D. Large-eddy simulation of low-frequency unsteadiness in a turbulent shock induced separation bubble. Theor Comput Fluid Dyn 2009, 23:79-107.
49. Wallin S., Johansson A.V. An explicit algebraic reynolds stress model for incompressible and compressible turbulent flows. J Fluid Mech 2000, 403:80-132.
50. Welch P.D. The use of fast fourier transform for the estimation of power spectra: a method based on time averaging over short, modified periodograms. IEEE Trans Audio Electroacoust AU-15 1967, 70-73.
51. Wilcox DC. Turbulence modeling for CFD. DCW Industries; 1998.
52. Wilcox D.C. Formulation of the k-ω turbulence model revisited. AIAA J 2009, 46(11):2823-2838.
53. Xiaoi X., Edwards J.R., Hassan H.A., Baurle R.A. Inflow boundary conditions for hybrid large-eddy/reynolds-averaged Navier-Stokes simulations. AIAA J 2003, 41(8):1481-1490.
54. Zhang Q., Schröder W., Meinke M. A zonal RANS/LES method to determine the flow over a high-lift configuration. Comput Fluids 2010, 39:1241-1253.
55. Zheltovodov A.A. Advances and problems in modelling of shock wave turbulent boundary layer interactions. Int Conf Methods Aerophys Res Part 2004, 2:149-157.