. Ph, L. Reijasse, D. Morzenski, J. Blacodon, and . Birkemeyer, Flow separation experimental analysis in overexpanded subscale rocket-nozzles, 37th AIAA/ASME/SEA/ASEE Joint Propuslion Conference and Exhibit, 2001.

A. Gross and C. Weiland, Investigation of shock patterns and separation behavior of several subscale nozzles AIAA-Paper Décollement de l'´ ecoulement externe induit par l'´ eclatement du jet propulsif sur un rétreint darrì ere-corps de missile, Ph. Reijasse, B. Corbel, 1998.

P. Servel, . Ph, R. Reijasse, and B. Benay, Etudes fondamentales sur les aspects aérodynamiques et thermiques desécoulementsàdesécoulements desécoulementsà larrì ere-corps des missiles. ONERA, Technical Note, 1998.

S. Moreau and T. Mauffret, Numerical simulations of afterbody flowfileds with two-equation turbulence models, 1996.

&. Conference, . Exhibit, and . Paper, References 1 SIMULOG, N3S-Natur V1.4, logiciel 3D Navier-Stokes, " Logiciel, manuels théorique, utilisateur et informatique, pp.10-13, 2001.

M. Dyke, An Album of Fluid Motion, 1982.

J. Ostlund, M. Damgaard, M. Frey, M. Frey, G. Hagemann et al., Side-load phenomena in highly over-expanded rocket nozzles AIAA Paper Status of flow separation prediction in rocket nozzles AIAA Paper 98-3619 Flow Separation ans Side-Loads in Rocket Nozzles Flow separation and side-loads in rocket nozzles, Proc. of the 4th Int. Symp. on Liquid Space Propulsion, 1998.

F. Nasuti, M. Onofri, and E. Pietropaoli, The influence of nozzle shape on the shock structure in separated flows, Proc. of the 5 th European Symposium on Aerothermodynamics of Space Vehicles, pp.353-358, 2004.

P. Reijasse, M. Frey, O. F. Haidn, S. Park, J. J. Kwon et al., Flow physics and side-loads in highly over-expanded rocket nozzles Zonal two equation k ? ? turbulence models for aerodynamic flows AIAA Paper 93-2906 Implementation of k ? ? turbulence models in an implicit multigrid method Realizability in two-equation turbulence models Investigation of shock patterns and separation behaviour of several subscales nozzles Computation and flow visualization in high-speed aerodynamics, Proc. of the ONERA/DLR Aerospace Symposium ODAS 2000, pp.1348-1357, 1993.

P. 15-reijasse, L. Morzenski, D. Blacodon, J. Birkemeyer, . Aiaa et al., Flow separation experimental analysis in overexpanded subscale rocket-nozzles Unsteadiness and side-loads in over-expanded supersonic nozzles Description of nozzle test cases Compressibility Effects in Turbulent Shear Layers, Proc. of the 4th European Symposium on Aerothermodynamics for Space Vehicles, pp.15-18, 1983.

D. Papamoschou and A. Roshko, The compressible turbulent shear layer: an experimental study, Journal of Fluid Mechanics, vol.23, issue.-1, pp.453-477, 1988.
DOI : 10.1017/S0022112058000653

. Schéma, Les tétraèdres T sont divisés en construisant autour de chacun de leur sommet un hexaèdre H, dont les sommets sont les milieux des arêtes de T contenant i (M 1 , M 2 et M 3 ), les centres de gravité des faces T contenant i (G 1 , G 2 et G 3 ), le centre de gravité G de l'élément et le sommet i lui-même, La cellule volume fini C i est la réunion de tous les hexaèdres H i liés à i

F. Cellules-volume, i et C j construites autour des noeuds i et j en 2D. ? i et ? j : frontières des volumes de contrôle C i et C j . ? ij : Portion de frontière commune à ? i et ? j . M k : milieux des arêtes du triangle T k . G k : centre de gravité de T k, p.46

D. Champ-de-vitesse-axiale-de-la-tuyère, éponge" près de la sortie (en haut) et sans (en bas). Ici, seul le domaine résolu est montré, p.54

.. De-recouvrement, 8 : numéro de sous-domaine ; ZR : Zone, p.55

D. Montage-expérimental-de-la-tuyère, Il s'agit ici du modèle récent avec parois transparentes, p.59

T. Maillage-de-la-tuyère and .. Du-domaine-extérieur-(-r-s-?-4, 5 cm, R col = 1 cm et L = 14.8 cm), p.59

.. Maillage-de-la-tuyère-r2ch-et-du-domaine-extérieur-(-r-s-?-5, 65 cm, R col = 1 cm et L = 12.5 cm), p.70

A. De-la-tuyère, Corps complet (a) et coupe longitudinale (b), p.93

.. Interaction-de-chocs-dans-une-tuyère-supersonique-mach, Apparition d'un léger phénomène de carbuncle en aval du disque de, p.129

H. O. Amann, Experimental Study of the Starting Process in a Reflection Nozzle, Physics of Fluids, vol.12, issue.5, pp.150-153, 1967.
DOI : 10.1063/1.1692597

P. Ardonceau, Etude de l'interaction onde de choc -couche limite supersonique, 1981.

G. Ben-dor, M. Ivanov, E. I. Vasilev, and T. Elperin, Hysteresis processes in the regular reflection???Mach reflection transition in steady flows, Progress in Aerospace Sciences, pp.347-387, 2002.
DOI : 10.1016/S0376-0421(02)00009-X

D. W. Bogdanoff, Compressibility Effects in Turbulent Shear Layers, AIAA Journal, vol.21, issue.6, pp.926-927, 1983.
DOI : 10.2514/3.60135

J. P. Boris, F. F. Grinstein, E. S. Oran, and R. J. Kolbe, New insights into large eddy simulation, Fluid Dynamics Research, vol.10, issue.4-6, p.199, 1992.
DOI : 10.1016/0169-5983(92)90023-P
URL : http://www.dtic.mil/get-tr-doc/pdf?AD=ADA249424

S. Catris, Etude de contraintes et qualification de modèles à viscosité turbulente Ecole Nationale Supérieure de l'Aéronautique et de l, 1999.

S. Catris and B. Aupoix, Density corrections for turbulence models, Aerospace Science and Technology, vol.4, issue.1, pp.1-11, 2000.
DOI : 10.1016/S1270-9638(00)00112-7

C. Chen, S. Chakravarty, and C. Hung, Numerical investigation of separated nozzle flows, AIAA Journal, vol.32, issue.9
DOI : 10.2514/3.12181

K. Chien, Predictions of channel and boundary-layer flows with a low-Reynolds-number two-equation model of turbulence, 18th Aerospace Sciences Meeting, pp.33-38, 1982.
DOI : 10.2514/6.1980-134

A. Chpoun, D. Passerel, H. Li, and G. Ben-dor, Reconsideration of oblique shock wave reflections in steady flows. Part 1. Experimental investigation, Journal of Fluid Mechanics, vol.123, issue.-1, pp.19-35, 1995.
DOI : 10.1017/S0022112095003776

P. Comte and M. Lesieur, Large eddy simulation of compressible turbulent flows. Lecture series 1998-05, Advance in turbulent modeling, von Karman institute for fluid dynamics, 1998.
URL : https://hal.archives-ouvertes.fr/hal-00553200

F. Dabireau, Etude des transferts de chaleur aux parois dans les moteur-fusées, 2002.

J. Delery and J. G. Marvin, Shock Wave/Boundary Layer Interactions, AGARDograph, issue.280, 1986.
DOI : 10.1016/B978-012086430-0/50024-5

J. Deleuze, Structure d'une couche limite turbulente soumise à une onde de choc incidente, 1995.

G. Douay, Modélisation et étude numérique de la turbulence compressible en écoulement supersonique, 1994.

S. Dubos, Simulation des grandes échelles d'écoulements turbulents supersoniques, 2005.

J. P. Dussauge, P. Dupont, J. F. Debieve, J. C. Robinet, A. Dervieux et al., Instationnarités et structures à grandes échelles : cas des interactions choc/couche limite avec décollement. Recherche aéronautique sur le supersonique, Programmes et actes, pp.22-30, 2002.

G. Erlebacher, M. Y. Speziale, C. G. Hussaini, and T. A. Zang, Toward the large-eddy simulation of compressible turbulent flows, Journal of Fluid Mechanics, vol.181, issue.-1, pp.90-76, 1990.
DOI : 10.1017/S0022112087002167

J. R. Forsythe, Numerical computation of turbulent separated supersonic flowfield, 2000.

J. R. Forsythe, W. Z. Strang, and K. A. Hoffmann, Validation of several Reynolds-averaged turbulence models in a 3-D unstructured grid code, Fluids 2000 Conference and Exhibit, pp.0-2552, 2000.
DOI : 10.2514/6.2000-2552

R. P. Fraser, D. Wilkie, and P. Eisenklam, Investigation of supersonic flow separation in nozzles, ARCHIVE: Journal of Mechanical Engineering Science 1959-1982 (vols 1-23), vol.1, issue.3, 1959.
DOI : 10.1243/JMES_JOUR_1959_001_031_02

M. Frey, Behandlung von Strömungsproblemen in Raketendüsen bei Überexpansion, 2001.

M. Frey and G. Hagemann, Status of flow separation prediction in rocket nozzles, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, pp.98-3619, 1998.
DOI : 10.2514/6.1998-3619

M. Frey and G. Hagemann, Flow separation ans side-loads in rocket nozzles, AIAA Paper, pp.99-2815, 1999.

M. Frey, A. Preuss, G. Hagemann, S. Girard, T. Alziary-de-roquefort et al., Joint European Effort Towards Advanced Rocket Thrust Chamber Technology, Proc. of the 6th international symposium on Launcher Technologies, 2005.

C. Fureby and F. F. Grinstein, Monotonically Integrated Large Eddy Simulation of Free Shear Flows, AIAA Journal, vol.37, issue.5, p.544, 1999.
DOI : 10.2514/2.772

C. Fureby and F. F. Grinstein, Large Eddy Simulation of high Reynolds number free and wall bounded flows, pp.0-2307, 2000.

M. Germano, U. Piomelli, P. Moin, and W. H. Cabot, A dynamic subgrid???scale eddy viscosity model, Physics of Fluids A: Fluid Dynamics, vol.3, issue.7, pp.1760-1765, 1991.
DOI : 10.1063/1.857955

S. K. Godunov, A difference scheme for numerical computation of discontinuous solutions of equations of fluid dynamics, Math. Sbornik, vol.47, pp.271-306, 1959.

J. Gressier, Robustesse et précision des schémas décentrés pour des écoulements compressibles, Ecole Nationale Supérieure de l'Aéronautique et de l'Espace, 1999.

F. F. Grinstein and C. Fureby, Recent progress on MILES for high Reynolds-number flows, 2002.

A. Hadjadj, Analyse physique et simulation numérique des écoulements compressibles applications aux tuyères de propulseur, 1997.

G. Hagemann, M. Frey, and W. Koschel, Appearance of Restricted Shock Separation in Rocket Nozzles, Journal of Propulsion and Power, vol.18, issue.3, pp.577-584, 2002.
DOI : 10.2514/2.5971

G. Hagemann, M. Terhardt, M. Frey, P. Reijasse, M. Onofri et al., Flow separation and side-loads in rocket nozzles, Proc. of the 4th Int. Symp. on Liquid Space Propulsion, Lampoldshausen (Germany), 2000.

A. Hellsten, Some improvements in Menter's k-omega SST turbulence model, 29th AIAA, Fluid Dynamics Conference, pp.98-2554, 1997.
DOI : 10.2514/6.1998-2554

J. Jimenéz and P. Moin, The minimal flow unit in near-wall turbulence, Journal of Fluid Mechanics, vol.204, issue.-1, pp.213-240, 1991.
DOI : 10.1017/S0022112069000115

P. S. Klebanoff, Characteristics of the turbulence in a boundary layer with zero pressure gradient, 1954.

B. E. Launder and B. I. Sharma, Application of the energy-dissipation model of turbulence to the calcultation of flow near a spinning disc, Letters in Heat and Mass Transfer, vol.1, pp.131-138, 1974.

B. E. Launder and D. B. Spalding, The numerical computation of turbulent flows, Computer Methods in Applied Mechanics and Engineering, vol.3, issue.2, pp.269-289, 1974.
DOI : 10.1016/0045-7825(74)90029-2

H. Laurent, Turbulence d'une interaction onde de choc/couche limite sur une paroi plane adiabatique ou chauffée, 1996.

R. A. Lawrence, Symmetrical and unsymmetrical separation in supersonic nozzles, Research Report, vol.671, 1967.

B. Van-leer, Towards the ultimate conservative difference scheme. II. Monotonicity and conservation combined in a second-order scheme, Journal of Computational Physics, vol.14, issue.4, 1974.
DOI : 10.1016/0021-9991(74)90019-9

A. Leonard, Energy Cascade in Large-Eddy Simulations of Turbulent Fluid Flows, Adv. Geophys, 1974.
DOI : 10.1016/S0065-2687(08)60464-1

T. D. Mckenney, Flow separation in overexpanded supersonic nozzles, ARS J, vol.320, 1954.

F. R. Menter, Zonal Two Equation k-w Turbulence Models For Aerodynamic Flows, 23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference, pp.93-2906, 1993.
DOI : 10.2514/6.1993-2906

O. Métais and M. Lesieur, Spectral large-eddy simulation of isotropic and stably stratified turbulence, Journal of Fluid Mechanics, vol.91, issue.-1, pp.157-194, 1992.
DOI : 10.1175/1520-0469(1976)033 2.0.CO;2

P. Moin, K. Squires, W. Cabot, and S. Lee, A dynamic subgrid???scale model for compressible turbulence and scalar transport, Physics of Fluids A: Fluid Dynamics, vol.3, issue.11, pp.2746-2757, 1991.
DOI : 10.1063/1.858164

J. G. Moore and J. Moore, Realizability in two-equation turbulence models, 30th Fluid Dynamics Conference, pp.99-3779, 1996.
DOI : 10.2514/6.1999-3779

M. V. Morkovin, Effect of compressibility on turbulent flows, Mécanique de la Turbulence, p.367, 1961.

F. Nasuti, M. Onofri, and E. Pietropaoli, The influence of nozzle shape on the shock structure in separated flows, Proc. of the 5 th European Symposium on Aerothermodynamics of Space Vehicles, pp.353-358, 2004.

L. H. Nave and G. A. Coffey, Sea level side loads in high-area-ratio rocket engines, 9th Propulsion Conference, pp.73-1284, 1973.
DOI : 10.2514/6.1973-1284

F. Nicoud and F. Ducros, Subgrid-scale stress modelling based on the square of the velocity gradient tensor. Flow, Turbulence and Combustion, pp.183-200, 1999.
URL : https://hal.archives-ouvertes.fr/hal-00910373

N. V. Nikitin, F. Nicoud, B. Wasistho, K. D. Squires, and P. R. Spalart, An approach to wall modeling in large-eddy simulations, Physics of Fluids, vol.12, issue.7, p.1629, 2000.
DOI : 10.1063/1.870414
URL : https://hal.archives-ouvertes.fr/hal-00910295

J. Ostlund, Flow processes in rocket engine nozzles with focus on flow separation and side-loads, Royal Institute of Technology, 2002.

D. Papamoschou, Noise Suppression in Moderate-Speed Multistream Jets, 8th AIAA/CEAS Aeroacoustics Conference & Exhibit, 2002.
DOI : 10.2514/6.2002-2557

D. Papamoschou and A. Roshko, The compressible turbulent shear layer: an experimental study, Journal of Fluid Mechanics, vol.23, issue.-1, pp.453-477, 1988.
DOI : 10.1017/S0022112058000653

S. H. Park and J. H. Kwon, Implementation of k-w Turbulence Models in an Implicit Multigrid Method, AIAA Journal, vol.42, issue.7, pp.1348-1357, 2004.
DOI : 10.2514/1.2461

C. Patel, W. Rodi, and G. Scheuerer, Turbulence models for near-wall and low Reynolds number flows - A review, AIAA Journal, vol.23, issue.9, pp.1308-1319, 1985.
DOI : 10.2514/3.9086

C. Pilinski, Etude numérique du décollement en tuyères supersoniques, 2002.

U. Piomelli, E. Balaras, M. Strelets, and P. R. Spalart, The inner???outer layer interface in large-eddy simulations with wall-layer models, International Journal of Heat and Fluid Flow, vol.24, issue.4, pp.538-550, 2003.
DOI : 10.1016/S0142-727X(03)00048-1

. Ph, B. Reijasse, and . Corbel, Décollement de l'écoulement externe induit par l'éclatement du jet propulsif sur un rétreint d'arrière-corps de missile. 34ème Colloque d'Aérodynamique Appliquée de l'AAAF, 1998.

P. L. Roe, Approximate Riemann solvers, parameter vectors, and difference schemes, Journal of Computational Physics, vol.43, issue.2, pp.357-372, 1981.
DOI : 10.1016/0021-9991(81)90128-5
URL : http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.457.5978

R. Sanders, E. Morano, and M. Druguet, Multidimensional Dissipation for Upwind Schemes: Stability and Applications to Gas Dynamics, Journal of Computational Physics, vol.145, issue.2, pp.511-537, 1998.
DOI : 10.1006/jcph.1998.6047

S. Sarkar, The stabilizing effect of compressibility in turbulent shear flow, Journal of Fluid Mechanics, vol.2, issue.-1, pp.163-186, 1995.
DOI : 10.1146/annurev.fl.23.010191.000543

S. Sarkar, G. Erlebacher, and M. Y. Hussaini, Compressible Homogeneous Shear: Simulation and Modeling, Proc. of the 8 th Symposium on Turbulent Shear Flows, pp.249-267, 1992.
DOI : 10.1007/978-3-642-77674-8_18
URL : http://www.dtic.mil/get-tr-doc/pdf?AD=ADA248141

P. Servel, . Ph, R. Reijasse, B. Benay, and . Corbel, Etudes fondamentales sur les aspects aérodynamiques et thermiques des écoulements à l'arrière-corps des missiles. ONERA, Technical Note, 1998.

M. Shur, P. R. Spalart, M. Strelets, and A. Travin, Detached-eddy simulation of an airfoil at high angle of attack, Proc. of the 4 th Int. Symp. Eng. Turb. Modelling and Measurements, 1999.
DOI : 10.1016/B978-008043328-8/50064-3

P. E. Skare and P. Krogstad, A turbulent equilibrium boundary layer near separation, Journal of Fluid Mechanics, vol.17, issue.-1, pp.319-348, 1994.
DOI : 10.1002/fld.1650090806

P. R. Spalart and S. R. Allmaras, A one-equation turbulence model for aerodynamic flows, 30th Aerospace Sciences Meeting and Exhibit, pp.5-21, 1994.
DOI : 10.2514/6.1992-439

P. R. Spalart, W. H. Jou, M. Strelets, and S. R. Allmaras, Comments on the feasibility of LES for wings and on a hybrid RANS/LES approach, 1997.

Y. B. Suzen and K. A. Hoffmann, Inverstigation of supersonic jet exhaust flow by one-and two-equation turbulence models, pp.98-0322, 1998.

D. Vandromme, H. Ha-minh, J. R. Viegas, M. W. Rubesin, and W. Kollmann, Second order closure for the calculation of compressible wall bounded flows with an implicit Navier-Stokes solver, 4th Symp. on Turbulent Shear Flows, 1983.

B. Vreman, B. Geurts, and H. Kuerten, Subgrid-modelling in LES of compressible flow, Applied Scientific Research, vol.4, issue.3, pp.191-203, 1995.
DOI : 10.1007/BF00849116