ACTION ITALO-FRANCAISE "PISA-INRIA"





Simulation et controle d'écoulements instationnaires turbulents et multiphasiques

Partenaires:

Dip. Ingegneria Aerospaziale, Universita di Pisa (I),

Scuola Normale Superiore, Pisa (I)

INRIA, projet Smash (F)


Coopération soutenue par la région Provence-Alpes Cote d'Azur

Calculs sur grille soutenues par l'ACI MECAGRID

Calculs coté Francais réalisés au CINES (Montpellier)

Quelques publications:

[1] I. ABALAKIN, M. BRAZA, S. CAMARRI, A. DERVIEUX, B. KOOBUS, T. KOZUBSKAYA, P. RODES, M.-V. SALVETTI, Unstable and unsteady aerodynamics : compared information from different numerical models, INRIA research report, 4077, 2000, in ``Fluid Dynamics and Aeronautics: new challenges'', J. Péeriaux, M. Champion, J.-J. Gagnepain. O. Pironneau, B. Stoufflet, P. Thomas Eds., CIMNE, Barcelona, 253-277, 2003 (Proceeeding of NFD 2000, Paris, 2001)

[2] S. CAMARRI, M.V. SALVETTI, B. KOOBUS, A. DERVIEUX, ``Large-eddy simulation of a bluff-body flow on unstructured grids'', Int. J. for Num. Meth. in Fluids, {40}, 1431-1460, (2002)

[3] S. CAMARRI, B. KOOBUS, M.V. SALVETTI, A. DERVIEUX, A low-diffusion MUSCL scheme for LES on unstructured grids, Computers and Fluids, Vol.33. 1101-1129, 2004

[4] B. KOOBUS, C. FARHAT, ``VMS Method for LES'', Comp. Meth. in Applied Math. and Eng.193, 1367-1383, 2004

[5] E. SINIBALDI, F. BEUX, M.-V. SALVETTI, A Preconditioned implicit Roe's scheme for barotropic flows: towards simulation of cavitation phenomena", INRIA RR-4891, 2003.

[6] E. SINIBALDI, F. BEUX, M.-V. SALVETTI, L. d'AGOSTINO, Numerical experiments with an homogeneous-flow model for thermal cavitation, Cav2003 Fifth International Symposium on Cavitation, 1-4 November 2003, Osaka.

[7] F. BEUX, M.V. SALVETTI, A. IGNATYEV, D. LI, C. MERKLE, E. SINIBALDI, A numerical study of non-cavitating and cavitating liquid flow around a hydrofoil, Mathematical Modelling and Numerical Analysis, 39/3, 577-590 (2005).

[8] E. SINIBALDI, F. BEUX, M.V. SALVETTI, A numerical method for 3D barotropic flows in turbomachinery, soumis a Journal of Flow, Turbulence and Combustion, Springer.

[9] E. SINIBALDI, F. BEUX, M.V. SALVETTI, A preconditioned compressible flow solver for numerical simulation of 3D cavitation phenomena, ECCOMAS 2004, 4th European Congress on Computational Methods in Applied Sciences and Engineering, 24-28 July 2004, Jyvaskyla, Finland.

[10] E. SINIBALDI, F. BEUX, A linearised implicit Roe scheme for inhomogeneous flux functions, 7th Congress of SIMAI, 20-24 september 2004, Venice, Italy.

[11] LOMA, Mathematical and Numerical aspects of Low Mach Number Flows, June 21-25, 2004 / Porquerolles, France.

[12] ECCOMAS 2004, 4th European Congress on Computational Methods in Applied Sciences and Engineering}, 24-28 July 2004, Jyvaskyla, Finland

[13] 7th Congress of SIMAI, 20-24 september 2004, Venice, Italy.

[14] Multiphase05, Conference on Numerical Simulation of Complex and Multiphase Flows, April 2005, IGESA Porquerolles, France.April 2005, IGESA Porquerolles, France.

[15] S. CAMARRI, M.V. SALVETTI, B. KOOBUS, A. DERVIEUX, ``A hybrid RANS/LES approach applied to bluff-body flow simulation'' ,Proceedings of IV European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS 2004, P. Neittaanmaki, T. Rossi, K. Majava and O. Pironneau Eds., Luglio 2004.

[16] V. MARIOTTI, S. CAMARRI, M.V. SALVETTI, B. KOOBUS, A. DERVIEUX, H. GUILLARD, S. WORNOM, "Numerical simulation of a jet in crossflow. Application to GRID computing", INRIA reoprt, to appear (2005).


Figures:

Supersonic Business Jet - Dassault Aviation: vortex shedding predicted with a LES model

LES past a square cylinder: level of turbulent viscosity

Isocontours du nombre de Mach dans l'ecoulement cavitant autour d'un profil d'aile NACA0015

Regions d'utilisations des differents modeles dans la simulation hybride d'un jet en ecoulement lateral

Iso-surfaces du module de vorticite dans l'ecoulement autour d'un prisme triangulaire (simulation LES)


Supersonic Business Jet - Dassault Aviation: vortex shedding predicted with a LES model

LES past a square cylinder: level of turbulent viscosity



Isocontours du nombre de Mach dans l'ecoulement cavitant autour d'un profil d'aile NACA0015 
Regions d'utilisations des differents modeles dans la simulation hybride d'un jet en ecoulement lateral 
Iso-surfaces du module de vorticite dans l'ecoulement autour d'un prisme triangulaire (simulation LES)





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