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BIBLIOGRAPHIE MENEVEAU, C. & KATZ, J. 2000 Scale-invariance and turbulence models for large eddy simulation. Annu. Rev. Fluid Mech. 32, 1–32. MENON, S. & N., PATEL 2006 Subgrid modeling for simulation of spray combustion in large scale combustors. AIAA J. 44 (709-723). MESSAADI, A. 2003 Etude des échanges convectifs le long d’une paroi à multiperforation inclinée. Application au refroidissement des parois des chambres de combustion. Thèse d’Université, Université de Poitiers. MÉTAIS, O. & LESIEUR, M. 1992 Spectral large-eddy simulation of isotropic and stably stratified turbulence. J. Fluid Mech. 239, 157–194. METZGER, D. E., TAKEUCHI, D. I. & KUENSTLER, P. A. 1973 Effectiveness and heat transfer with full-coverage film-cooling. ASME paper . MIAO, JR-MING & CHING, HONG-KA 2006 Numerical simulation of film-cooling concave plate as coolant jet passes through two rows of holes with various orientations of coolant flow. Int. J. Heat Mass Transf. 49, 557–574. MICHEL, B., GAJAN, P., STRZELECKI, A., KOURTA, A. & BOISSON, H. 2007 Simulation numérique d’une zone d’injection pariétale pour une chambre de combustion de turbomachine. In 18ème Congrès Français de Mécanique. Grenoble, août 2007. MIRON, P. 2005 Étude expérimentale des lois de parois et du film de refroidissement produit par une zone multiperforée sur une paroi plane. Thèse d’Université, Université de Pau et des Pays de l’Adour. MOFFAT, R. J. & KAYS, W. M. 1968 The turbulent boundary layer on a porous plate : experimental heat transfer with uniform blowing and suction. Int. J. Heat Mass Transf. 11, 1547–1566. MOIN, P. 2004 Large eddy simulation of multi-phase turbulent flows in realistic combustors. Prog. Comput. Fluid Dynamics 4, 237–240. MOIN, P. & APTE, S. V. 2006 Large-eddy simulation of realistic gas turbine combustors. AIAA J. 44 (4), 698–708. MOIN, P. & KIM, J. 1982 Numerical investigation of turbulent channel flow. J. Fluid Mech. 118, 341– 377. MOIN, P. & MAHESH, K. 1998 Direct numerical simulation : A tool in turbulence research. Annu. Rev. Fluid Mech. 30 (539-578). MOIN, P., SQUIRES, K., CABOT, W. & LEE, S. 1991 A dynamic subgrid-scale model for compressible turbulence and scalar transport. Phys. FluidsA 3 (11), 2746–2757. MOST, A. 2007 Etude expérimentale et numérique du film de refroidissement produit par l’injection pariétale d’air au travers d’une paroi multiperforée. Thèse d’Université, Université de Pau et des Pays de l’Adour. 188
BIBLIOGRAPHIE MOST, A. & BRUEL, P. 2007 Numerical assessment of jet trajectories analysis in film cooling systems. In 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. MOST, A., SAVARY, N. & BÉRAT, C. 2007 Reactive flow modelling of a combustion chamber with a multiperforated liner. In 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. MULDOON, F. & ACHARYA, S. 2006 Analysis of k and epsilon budgets for film cooling using direct numerical simulation. AIAA J. 44 (12), 3010–3021. MUPPIDI, S. & MAHESH, K. 2005 Study of trajectories of jets in crossflow using direct numerical simulations. J. Fluid Mech. 530, 81–100. MUPPIDI, S. & MAHESH, K. 2006 Two-dimensional model problem to explain counter-rotating vortex pair formation in a transverse jet. Phys. Fluids 18 (8). MUPPIDI, S. & MAHESH, K. 2007 Direct numerical simulation of round turbulent jets in crossflow. J. Fluid Mech. 574, 59–84. NASIR, H., ACHARYA, S. & EKKAD, S. 2003 Improved film cooling from cylindrical angled holes with triangular tabs : effect of tab orientations. Int. J. Heat Fluid Flow 24, 657–668. NGUYEN-PHU, H. 2006 Etude des échanges convectifs à l’entrée d’une perforation : Application à la thermique des parois multiperforées des chambres de combustion. Thèse d’Université, Université de Poitiers. NICOUD, F. & DUCROS, F. 1999 Subgrid-scale stress modelling based on the square of the velocity gradient tensor. Flow Turbul. Combust. 62 (3), 183–200. PAPANICOLAOU, E., GIEBERT, D., KOCH, R. & SCHULTZ, A. 2001 A conservation-based discretization approach for conjugate heat transfer calculations in hot-gas ducting turbomachinery components. Int. J. Heat Mass Transf. 44, 3413–3429. PEET, Y. V. 2006 Film cooling from inclined cylindrical holes using Large-Eddy Simulations. Thèse d’Université, Stanford University. PETERSON, S. D. & PLESNIAK, M. W. 2002 Short-hole jet-in-crossflow velocity field and its relationship to film-cooling performance. Exps. Fluids 33, 889–898. PETERSON, S. D. & PLESNIAK, M. W. 2004a Evolution of jets emanating from short holes into crossflow. J. Fluid Mech. 503, 57–91. PETERSON, S. D. & PLESNIAK, M. W. 2004b Surface shear stress measurements around multiple jets in crossflow using the fringe imaging skin friction technique. Exps. Fluids 37, 497–503. PETRE, B. 2001 Étude des échanges convectifs en espace confiné le long d’une paroi multiperforée. Thèse d’Université, Université de Poitiers. ENSMA. PIETRZYK, J. R., BOGARD, D. G. & CRAWFORD, M. E. 1989 Hydrodynamic measurements of jets in crossflow for gas turbine film cooling applications. ASME J. Turbomach. 111, 139–145. 189
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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,
Page 137 and 138: 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: BIBLIOGRAPHIE LIEUWEN, T. & YANG, V
Page 191 and 192: BIBLIOGRAPHIE SCHILDKNECHT, M., MIL
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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