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BIBLIOGRAPHIE PIOMELLI, U. & BALARAS, E. 2002 Wall-layer models for large-eddy simulations. Annu. Rev. Fluid Mech. 14, 349–374. PITSCH, H. 2006 Large eddy simulation of turbulent combustion. Annu. Rev. Fluid Mech. 38, 453–482. PLESNIAK, M. W. 2006 Noncanonical short hole jets-in-crossflow for turbine film cooling. J. Applied Mechanics 73 (3), 474–482. POINSOT, T. & LELE, S. K. 1992 Boundary conditions for direct simulations of compressible viscous flows. J. Comput. Phys. vol.101 (1), 104–129. POINSOT, T. & VEYNANTE, D. 2001 Theoretical and Numerical Combustion. Edwards. POPE, S. B. 2000 Turbulent flows. Cambridge University Press. POPE, S. B. 2004 Ten questions concerning the large-eddy simulation of turbulent flows. New Journal of Physics 6, 35. PORTA, M. 2007 Développement, vérification et validation des outils les pour l’étude du bruit de combustion et de l’interaction combustion/acoustique/turbulence. Thèse d’Université, INP Toulouse. RENZE, P., SCHRÖDER, W. & MEINKE, M. 2007 LES of film cooling efficiency for different hole shapes. In 5th Symposium on Turbulent and Shear Flow Phenomena. Munich, Germany. REYNOLDS, W. C. 1989 The potential and limitations of direct and large eddy simulations. In Whither Turbulence workshop, Cornell University, March 22-24. RICHARDSON, L.F. 1922 Weather Prediction by Numerical Process. Cambridge University Press. RIVERO, A., FERRÉ, J. A. & GIRALT, F. 2001 Organized motions in a jet in crossflow. J. Fluid Mech. 444, 117–149. ROGALLO, R. & MOIN, P. 1985 Numerical simulation of turbulent flows. Annu. Rev. Fluid Mech. 17, 99–137. ROUVREAU, S. 2001 Étude expérimentale de la structure moyenne et instantanée d’un film produit par une zone multiperforée sur une paroi plane. application au refroidissement des chambres de combustion des moteurs aéronautiques. Thèse d’Université, E.N.S.M.A. et Faculté des Sciences Fondamentales et Appliquées. ROUX, S., CAZALENS, M. & T., POINSOT 2007 Influence of outlet boundary condition for large eddy simulation of combustion instabilities in gas turbine. submitted to AIAA J. . ROUX, S., LARTIGUE, G., POINSOT, T., MEIER, U. & BÉRAT, C. 2005 Studies of mean and unsteady flow in a swirled combustor using experiments, acoustic analysis and large eddy simulations. Combust. Flame 141, 40–54. SAGAUT, P. 2002 Large eddy simulation for incompressible flows. Springer. SANKARAN, V. & MENON, S. 2002 Les of spray combustion in swirling flows. J. Turb. 3, 011. 190
BIBLIOGRAPHIE SCHILDKNECHT, M., MILLER, J. A. & MEIER, G. E. A. 1979 The influence of suction on the structure of turbulence in fully developed pipe flow. J. Fluid Mech. 90, 67–107. SCHLICHTING, H. & GERSTEN, K. 2000 Boundary layer theory, 8th edn. Springer-Verlag. SCHMITT, P., POINSOT, T., SCHUERMANS, B. & GEIGLE, K. 2007 Large-eddy simulation and experimental study of heat transfer, nitric oxide emissions and combustion instability in a swirled turbulent high-pressure burner. J. Fluid Mech. 570, 17–46. SCHÖNFELD, T. & RUDGYARD, M. 1999 Steady and unsteady flows simulations using the hybrid flow solver AVBP. AIAA J. 37 (11), 1378–1385. SCRITTORE, J. J., THOLE, K. A. & BURD, S. W. 2007 Investigation of velocity profiles for effusion cooling of a combustor liner. ASME J. Turbomach. 129, 518–526. SENGISSEN, A., VANKAMPEN, J. F., HULS, R., STOFFELS, G., KOK, J. B. W. & POINSOT, T. 2007 LES and experimental studies of cold and reacting flows in a swirled partially premixed burner with and without fuel modulation. Combust. Flame 150, 40–53. SENSIAU, C., NICOUD, F., GICQUEL, L. Y. M., POINSOT, T. & MOUREAU, V. 2007 Acoustic analysis of industrial gas turbines. In 11th CEAS-ASC Workshop and 2nd Scientific Workshop of X3-NOISE 27– 28 September 2007, Lisbon, Portugal. SILVA-FREIRE, A. P., CRUZ, D. O. A. & PELLEGRINI, C. C. 1995 Velocity and temperature distributions in compressible turbulent boundary layers with heat and mass transfer. Int. J. Heat Mass Transf. 38 (13), 2507—2515. SIMPSON, R. L. 1970 Characteristics of turbulent boundary layers at low reynolds numbers with and without transpiration. J. Fluid Mech. 42 (4), 769–802. SINHA, A. K., BOGARD, D. G. & CRAWFORD, M. E. 1991 Film-cooling effectiveness downstream of a single row of holes with variable density ratio. ASME J. Turbomach. 113, 442–449. SMAGORINSKY, J. 1963 General circulation experiments with the primitive equations : I. the basic experiment. Monthly Weather Review 91, 99–164. SMITH, S. H. & MUNGAL, M. G. 1998 Mixing, structure and scaling of the jet in crossflow. J. Fluid Mech. 357, 83–122. SPARROW, E. M. & CARRANCO ORTIZ, M. 1982 Heat transfer coefficients for the upstream face of a perforated plate positioned normal to an oncoming flow. Int. J. Heat Mass Transf. 25 (1), 127–135. SPARROW, E. M. & GURDAL, U. 1981 Heat transfer at an upstream-facing surface washed by fluid en route to an aperture in the surface. Int. J. Heat Mass Transf. 24 (5), 851–857. STAFFELBACH, G., BOUDIER, G., LAMARQUE, N., SENSIAU, C., GICQUEL, L. Y. M., POINSOT, T. & MOUREAU, V. 2007 Azimuthal thermo-acoustic stability of a full gas turbine combustion chamber using large-eddy simulations. In 11th CEAS-ASC Workshop and 2nd Scientific Workshop of X3-NOISE 27–28 September 2007, Lisbon, Portugal. 191
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UNIVERSITE MONTPELLIER II SCIENCES
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Table des matières Remerciements 7
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Remerciements Cette thèse a été
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Liste des symboles Lettres romaines
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Introduction générale La volonté
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Chapitre 1 Contexte industriel et s
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1.1 Les turbines à gaz pour les tu
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1.1 Les turbines à gaz a) b) GAZ C
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1.2 La simulation numérique des é
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1.3 Objectifs et plan de la thèse
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Chapitre 2 L’écoulement autour d
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2.1 Présentation de la configurati
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2.2 Perte de charge au passage d’
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2.3 La multi-perforation : aspects
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2.4 Caractérisation aérodynamique
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2.5 Modélisation de la multi-perfo
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Chapitre 3 Simulations des grandes
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3.2 Simulations des Grandes Echelle
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3.3 Le code de calcul AVBP 3.3.1 As
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3.3 Le code de calcul AVBP dans le
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3.3 Le code de calcul AVBP de sa st
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Chapitre 4 Simulations numériques
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4.1 Quelles simulations pour la mod
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4.2 Choix de la méthode de simulat
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4.2 Choix de la méthode de simulat
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4.3 Sensibilité des simulations au
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Chapitre 5 Simulations numériques
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2 S. Mendez and F. Nicoud COMBUSTIO
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4 S. Mendez and F. Nicoud (c) The i
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6 S. Mendez and F. Nicoud CALCULATI
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8 S. Mendez and F. Nicoud Name Numb
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10 S. Mendez and F. Nicoud x/d z/d
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12 S. Mendez and F. Nicoud main, it
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14 S. Mendez and F. Nicoud 1.0 a 1.
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16 S. Mendez and F. Nicoud ROWS 1 3
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18 S. Mendez and F. Nicoud Figure 1
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20 S. Mendez and F. Nicoud 30 ◦ 3
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22 S. Mendez and F. Nicoud & Mahesh
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28 S. Mendez and F. Nicoud film, th
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30 S. Mendez and F. Nicoud Region t
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32 S. Mendez and F. Nicoud Expressi
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34 S. Mendez and F. Nicoud geometri
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36 S. Mendez and F. Nicoud (f) Two
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38 S. Mendez and F. Nicoud Mendez,
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Chapitre 6 Un modèle adiabatique p
Page 139 and 140: ρ Mass density, kg/m 3 P T V i τ
Page 141 and 142: cence of the jets. This is particul
Page 143 and 144: Simulations. The small-scale LES re
Page 145 and 146: chosen to compare with numerical re
Page 147 and 148: pressure drop of 41 Pa is effective
Page 149 and 150: Region total plate hole solid wall
Page 151 and 152: This equality is almost verified at
Page 153 and 154: V U σ V inj jet cotan(α′ ) V U
Page 155 and 156: PERIODIC Z INFLOW 1 WALL 24 OUTFLOW
Page 157 and 158: part of the plate. Downstream of th
Page 159 and 160: streamwise momentum flux. As a cons
Page 161 and 162: 8 Fric, T. and Roshko, A., “Vorti
Page 163 and 164: Discussion sur la modélisation de
Page 165 and 166: 20 15 10 y/d 5 0 -5 -10 0.0 0.2 0.4
Page 167 and 168: Chapitre 7 Simulations numériques
Page 169 and 170: Primary flow (burnt gases) Secondar
Page 171 and 172: Figure 7: Nusselt number over the s
Page 173 and 174: the perforated plate. A Large-Eddy
Page 175 and 176: Les tableaux de flux permettent de
Page 177 and 178: Conclusion générale Dans cette é
Page 179 and 180: Conclusion générale En ce qui con
Page 181 and 182: Bibliographie AKSELVOLL, K. & MOIN,
Page 183 and 184: BIBLIOGRAPHIE CORON, X. 2001 Étude
Page 185 and 186: BIBLIOGRAPHIE HALE, C. A., PLESNIAK
Page 187 and 188: BIBLIOGRAPHIE LIEUWEN, T. & YANG, V
Page 189: BIBLIOGRAPHIE MOST, A. & BRUEL, P.
Page 193: Annexes
Page 196 and 197: ARTIFICIAL VISCOSITY MODELS A.2.1 T
Page 198 and 199: ARTIFICIAL VISCOSITY MODELS - 4 th
Page 200 and 201: ARTIFICIAL VISCOSITY MODELS As a co
Page 202: ARTIFICIAL VISCOSITY MODELS 202
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