Large Eddy simulation applied to a high-reynolds flow around an airfoil close to stall

41st Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2003, Pages

  Dahlstrom S ^a   Davidson, L ^a  

^a CHALMERS UNIVERSITY OF TECHNOLOGY   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; BOUNDARY LAYER FLOW; LAMINAR FLOW; LARGE EDDY SIMULATION; REYNOLDS NUMBER;

BOUNDARY LAYER THICKNESS; FLOW AROUND AN AIRFOIL; HIGH REYNOLDS NUMBER; LAMINAR SEPARATION BUBBLE; THREE-DIMENSIONAL BODY; TRANSITION MECHANISM; TURBULENT BOUNDARY LAYERS; UNPHYSICAL OSCILLATIONS;

LAMINAR BOUNDARY LAYER;

EID: 85085774292     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-776     Document Type: Conference Paper

References (28)

1. Davidson, L., "LESFOIL: an European Project on Large Eddy Simulations around a High-Lift Airfoil at High Reynolds Number, " ECCOMAS 2000, European Congress on Computational Methods in Applied Sciences and Engineering, 11-14 September, Barcelona, Spain, 2000.
2. Davidson, L., Cokljat, D., Fröhlich, J., Leschziner, M., Mellen, C., and Rodi, W., editors, LESFOIL-Large Eddy Simulation of Flow Around a High-Lift Airfoil, Springer, 2002, In preparation.
3. Mellen, C., Fröhlich, J., and Rodi, W., "Lessons from the European LESFOIL project on LES of flow around an airfoil, " 40th Aerospace Sciences Meeting, AIAA Paper 2002-0111, Reno, 2002.
4. Chaput, E., "Aerospatiale-A Airfoil. Contribution in ECARP-European Computational Aerodynamics Research Project: Validation of CFD Codes and Assessment of Turbulence Models, " Notes on Numerical Fluid Mechanics, edited by W. H. et al., Vol. 58, Vieweg Verlag, 1997, pp. 327-346.
5. Haase, W., Brandsma, F., Elsholz, E., Leschziner, M., and Schwamborn, D., editors, EUROVAL-A European Initiative on Validation of CFD-codes, Vol. 42, Vieweg Verlag, 1993.
6. Haase, W., Chaput, E., Elsholz, E., Leschziner, M., and Müller, U., editors, ECARP-European Computational Aerodynamics Research Project: Validation of CFD Codes and Assessment of Turbulence Models, Vol. 58, Vieweg Verlag, 1997.
7. Davidson, L. and Rizzi, A., "Navier-Stokes Stall Predictions Using an Algebraic Stress Model, " J. Spacecraft and Rockets, Vol. 29, 1992, pp. 794-800.
8. Davidson, L., "Prediction of the Flow Around an Airfoil Using a Reynolds Stress Transport Model, " ASME: Journal of Fluids Engineering, Vol. 117, 1995, pp. 50-57.
9. Lien, F. and Leschziner, M., "Modelling of 2D Separation from High-Lift Aerofoils With a Non-Linear Eddy-Viscosity Model and Second-Moment Closure, " The Aeronautical Journal, Vol. 99, 1995, pp. 125-144.
10. Kaltenbach, H.-J. and Choi, H., "Large-Eddy Simulation of Flow Around an Airfoil on a Structured Mesh, " Annual Research Briefs 1995, Center for Turbulent Research, Stanford Univ./NASA Ames Reseach Center, 1995, pp. 51-60.
11. Weber, C. and Ducros, F., "Large-eddy and Reynolds Averaged Navier-Stokes Simulations of turbulent flow over an airfoil, " Int. J. Comput. Fluid Dyn., Vol. 13, 2000, pp. 327-355.
12. Held, J., Large Eddy Simulation of Separated Compressible Flows around Wing Sections, Ph.D. thesis, Dept. of Heat and Power Engineering, Lund Institute of Technology, Lund, 1999.
13. Mary, I. and Sagaut, P., "Large Eddy Simulation of flow around an airfoil near stall, " AIAA Journal, Vol. 40, No. 6, 2002, pp. 1139-1145.
14. Mellen, C., Fröhlich, J., and Rodi, W., "Contribution by IfH in LESFOIL-Large Eddy Simulation of Flow Around a High-Lift Airfoil, " LESFOIL, edited by L. Davidson, D. Cokljat, J. Fröhlich, M. Leschziner, C. Mellen, and W. Rodi, Springer, 2002, In preparation.
15. Dahlström, S. and Davidson, L., "Large Eddy Simulation of the Flow around an Airfoil, " 39th Aerospace Sciences Meeting, AIAA Paper 2001-0425, Reno, 2001.
16. Voke, P., "Transition in LESFOIL-Large Eddy Simulation of Flow Around a High-Lift Airfoil, " LESFOIL, edited by L. Davidson, D. Cokljat, J. Fröhlich, M. Leschziner, C. Mellen, and W. Rodi, Springer, 2002, In preparation.
17. Cokljat, D. and Liu, F., "DES of turbulent flow over an airfoil at high incidence, " 40th Aerospace Sciences Meeting, AIAA Paper 2002-0590, Reno, 2002.
18. Dahlström, S. and Davidson, L., "Contribution by Chalmers in LESFOIL-Large Eddy Simulation of Flow Around a High-Lift Airfoil, " LESFOIL, edited by L. Davidson, D. Cokljat, J. Fröhlich, M. Leschziner, C. Mellen, and W. Rodi, Springer, 2002, In preparation.
19. Ducros, F., "Contribution by CERFACS in LESFOIL-Large Eddy Simulation of Flow Around a High-Lift Airfoil, " LESFOIL, edited by L. Davidson, D. Cokljat, J. Fröhlich, M. Leschziner, C. Mellen, and W. Rodi, Springer, 2002, In preparation.
20. Davidson, L. and Farhanieh, B., "CALC-BFC: A Finite-Volume Code Employing Collocated Variable Arrangement and Cartesian Velocity Components for Computation of Fluid Flow and Heat Transfer in Complex Three-Dimensional Geometries, " Rept. 95/11, Dept. of Thermo and Fluid Dynamics, Chalmers University of Technology, Gothenburg, 1995.
21. Rhie, C. and Chow, W., "Numerical Study of the Turbulent Flow Past an AirfoilWith Trailing Edge Separation, " AIAA Journal, Vol. 21, 1983, pp. 1525-1532.
22. Nilsson, H. and Davidson, L., "CALC-PVM: A Parallel Multiblock SIMPLE Multiblock Solver for Turbulent Flow in Complex Domains, " Tech. Rep. 98/12, Dept. of Thermo and Fluid Dynamics, Chalmers University of Technology, Gothenburg, 1998.
23. Issa, R., "Solution of Implicitly Discretised Fluid Flow Equations by Operator-Splitting, " J. Comp. Physics, Vol. 62, 1986, pp. 40-65.
24. Yoshizawa, A., "Statistical Theory for Compressible Shear Flows with the Application of Subgrid Modelling, " Physics of Fluids A, Vol. 29, 1986, pp. 2152-2163.
25. Fureby, C., "Large Eddy Simulation of Rearward-Facing Step Flow, " AIAA Journal, Vol. 37, No. 11, 1999, pp. 1401-1410.
26. Durbin, P. A., "On the k-3 stagnation point anomaly, " Int. J. Heat and Fluid Flow, Vol. 17, 1996, pp. 89-90.
27. Ferziger, J. and Peric, M., Computational Methods for Fluid Dynamics, Springer-Verlag, Berlin, 1996.
28. Davidson, L., "Hybrid LES-RANS: A Combination of a Oneequation SGS Model and a k-ω Model for predicting Recirculating Flows, " ECCOMAS CFD Conference, Swansea, U.K., 2001.