Large eddy simulation of vortex breakdown behind a delta wing

International Journal of Heat and Fluid Flow

Volumn 24, Issue 4, 2003, Pages 596-605

  Mary, I ^a  

^a ONERA   (France)

Author keywords

Delta wing; LES; Local mesh refinement; Semi structured grids; Vortex breakdown; Wall function

Indexed keywords

COMPUTER SIMULATION; REYNOLDS NUMBER; WIND TUNNELS; WINGS;

LARGE-EDDY SIMULATION (LES);

TURBULENT FLOW;

DELTA WING; LARGE EDDY SIMULATION; REYNOLDS NUMBER; TURBULENT FLOW; VORTEX; WALL;

EID: 0038208169     PISSN: 0142727X     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0142-727X(03)00053-5     Document Type: Article

References (18)

1. Batten, P., Goldberg, U.C., Palaniswamy, S., Chakravarthy, S.R., 2001. Hybrid RANS/LES: spatial-resolution and energy-transfer issues. In: Turbulent and Shear Flow Phenomena 2nd International Symposium, Stockolm, Sweden
2. Boris J.P. Grinstein F.F. Oran E.S. Kolbe R.L. New insights into large eddy simulation Fluid Dynam. Res. 10 1992 199-228
3. Davidson L., Cokljat D., Fröhlich J., Leschziner M., Mellen C., Rodi W. (Eds.), 2003. LESFOIL: LES of Flow Around a High Lift Airfoil. Notes on Numerical Fluid Mechanics, Vol. 83. Springer
4. Goncalves E. Houdeville R. Reassessment of the wall functions approach for RANS computations Aerosp. Sci. Technol. 5 2001 1-14
5. Guy, Y., Morrow, J.A., McLaughlin, T.A., Wygnanski, I., 2000. Parametric investigation of the effect of active control of the normal force on a delta wing. AIAA Paper 2000-0550
6. Larchevêque L. Sagaut P. Mary I. Labbé O. Comte P. LES of a compressible flow past a deep cavity Phys. Fluid 15 2003 193-210
7. Leibovitch S. The structure of vortex breakdown Ann. Rev. Fluid Mech. 10 1978 221-246
8. Lenormand E. Sagaut P. Ta Phuoc L. Large-eddy simulation of subsonic and supersonic channel flow at moderate Reynolds number Int. J. Numer. Meth. Fluids 32 2000 369-406
9. Leroy, G., Mary, I., 2001. PEA aérodynamique et mécanique du vol: Prédiction de l'éclatement tourbillonnaire sur une aile delta par la SGE. Rapport ONERA, RA 8/05284 DSNA
10. Mary I. Sagaut P. LES of flow around an airfoil near stall AIAA J. 40 2002 1139-1145
11. Mitchell, A., Molton, P., Barberis, D., Gobert, J.L., 2000a. Control of vortex breakdown by along-the-core blowing. AIAA Paper 2000-2608
12. Mitchell, A., Molton, P., Barberis, D., Délery, J., 2000b. Characterization of vortex breakdown by flow field and surface measurements. AIAA Paper 2000-0788
13. Molton, P., Barberis, D., Mitchell, A., 1999. Etude expérimentale de l'éclatement tourbillonnaire sur une aile delta de 70 degrés de flèche en écoulement incompressible. Analyse des répartitions de la pression pariétale. Rapport ONERA, RT 124/7078 DAFE/N
14. Nicoud F. Bagett J.S. Moin P. Cabot W. LES wall-modelling based on suboptimal control theory and linear stochastic estimation Phys. Fluids 13 2001 2968-2984
15. Péchier M. Guillen P. Gayzac R. Magnus effect over finned projectiles J. Spacecraft Rockets 38 2001 542-549
16. Quéméré P. Sagaut P. Couailler V. A new multi-domain/multi-resolution method for large eddy simulation Int. J. Numer. Meth. Fluids 36 2001 391-416
17. Schmidt, S., Franke, M., Thiele, F., 2001. Assessment of SGS models in LES applied to a naca 4412 airfoil. AIAA Paper 2001-0434
18. Werlé H. Sur l'éclatement des tourbillons d'apex d'une aile delta aux faibles vitesses La Rech. Aéronaut. 74 1960 23-30