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BIBLIOGRAPHIE VON KARMAN, T. 1934 Turbulence and skin friction. Journal of Aeronautical Sciences 1 (1). KASAGI, N., HIRATA, M. & KUMADA, M. 1981 Studies of full-coverage film cooling part 1 : Cooling effectiveness of thermally conductive wall. ASME Paper 81-GT-37 . KASZETA, R. W. 1998 Measurements in film cooling flows with lateral injection. Thèse d’Université, University of Minnesota. KELSO, R. M., LIM, T. T. & PERRY, A. E. 1996 An experimental study of round jets in cross-flow. J. Fluid Mech. 306, 111–144. KIM, J., MOIN, P. & MOSER, R. 1987 Turbulence statistics in fully developed channel flow at low Reynolds number. J. Fluid Mech. 177, 133–166. KIM, W.W., MENON, S. & MONGIA, H.C. 1999 Large-eddy simulation of a gas turbine combustor. Combust. sci. technol. 143 (1-6), 25–62. KOLMOGOROV, A.N. 1941 The local structure of turbulence in incompressible viscous fluid for very large reynolds numbers. C.R. Acad. Sci. USSR 30, 301. KUMADA, M., HIRATA, M. & KASAGI, N. 1981 Studies of full-coverage film cooling part 2 : Measurements of local heat transfer coefficient. ASME Paper 81-GT-38 . LAKSHMINARAYANA, B. 1996 Fluid Dynamics and Heat Transfer of Turbomachinery. Wiley. LAMARQUE, N. 2007 Schémas et conditions limites pour la simulation aux grandes échelles de la combustion diphasique dans les foyers d’hélicoptères. Thèse d’Université, INP Toulouse. LAX, P. D. & WENDROFF, B. 1960 Systems of conservation laws. Comm. Pure Appl. Math. 13, 217– 237. LEBROCQ, P. V., LAUNDER, B. E. & PRIDDIN, C. H. 1973 Discrete hole injection as a means of transpiration cooling ; an experimental study. Proc Instn Mech Engrs 187 (17), 149–157. LEFEBVRE, A. H. 1999 Gas Turbines Combustion. Taylor & Francis. LESIEUR, M. 1997 Recent approaches in large-eddy simulations of turbulence. In New tools in turbulence modelling (ed. O. Métais & J. Ferziger), pp. 1 – 28. Les Editions de Physique - Springer Verlag. LESIEUR, M. & MÉTAIS, O. 1996 New trends in large-eddy simulations of turbulence. Annu. Rev. Fluid Mech. 28, 45 – 82. LESIEUR, M., MÉTAIS, O. & COMTE, P. 2005 Large-Eddy Simulations of Turbulence. Cambridge University Press. LESIEUR, M., STAQUET, C., P., LEROY & COMTE, P. 1988 The mixing layer and its coherence examined from the point of view of two dimensionnal turbulence. J. Fluid Mech. 192, 511–534. LEYLEK, J. H. & ZERKLE, R. D. 1994 Discrete-jet film cooling : A comparison of computational results with experiments. ASME J. Turbomach. 116, 358–368. 186
BIBLIOGRAPHIE LIEUWEN, T. & YANG, V. 2005 Combustion instabilities in gas turbine engines. Operational experience, fundamental mechanisms and modeling. In Progress in Astronautics and Aeronautics AIAA, , vol. 210. LIGRANI, P.M., WIGLE, J.M., CIRIELLO, S. & JACKSON, S.M. 1994 Film-cooling from holes with compound angle orientations : part 1-results downstream of two staggered rows of holes with 3d spanwise spacing. J. Heat Transf. 116, 341–352. LILLY, D.K. 1967 The representation of small-scale turbulence in numerical simulation experiments. In Proceedings of the IBM Scientific Computing Symposium on Environmental Sciences. Yorktown Heights, USA. MACMANUS, D. G. & EATON, J. A. 2000 Flow physics of discrete boundary layer suction - measurements and predictions. J. Fluid Mech. 417, 47–75. MAHESH, K., CONSANTINESCU, G., APTE, S., IACCARINO, G. & MOIN, P. 2001 Large eddy simulation of gas turbine combustors. In Center for Turbulence Research, Annual Research Briefs, pp. 1–15. MARGASON, R. J. 1993 Fifty years of jet in crossflow research. In Computational and Experimental Assessment of Jets in Crossflow (ed. UK Winchester), , vol. AGARD-CP-534, pp. 1–41. MARTIN, R. 2006a N3S-NATUR V2.1, Manuel Utilisateur. SIMULOG. MARTIN, R. 2006b Projet N3S-NATUR V2.1, Manuel Theorique, Sotware Package. Simulog, France. MARTINY, M., SCHULTZ, A. & WITTIG, S. 1995 Full-coverage film cooling investigations : adiabatic wall temperatures and flow visualization. ASME paper 95-WA/HT-4 . MATTINGLY, J. D. 2005 Elements of gas turbine propulsion, 2nd edn. AIAA. MAYLE, R.E. & CAMARATA, F.J. 1975 Multihole cooling effectiveness and heat transfer. Transf. 97, 534–538. J. Heat MCGOVERN, K. T. & LEYLEK, J.H. 2000 A detailed analysis of film-cooling physics : Part 2- compound-angle injection with cylindrical holes. ASME J. Turbomach. 122, 113–121. MEDIC, G. & DURBIN, P. A. 2002 Toward improved film cooling prediction. ASME J. Turbomach. 124, 193–199. MENDEZ, S., ELDREDGE, J. D., NICOUD, F., POINSOT, T., SHOEYBI, M. & IACCARINO, G. 2006a Numerical investigation and preliminary modeling of a turbulent flow over a multi-perforated plate. In Proc. Summer Program CTR, NASA Ames - Stanford University. MENDEZ, S., NICOUD, F. & MIRON, P. 2005 Direct and large-eddy simulations of a turbulent flow with effusion. In ERCOFTAC WORKSHOP. Direct and Large-Eddy Simulations 6. Poitiers FRANCE. MENDEZ, S., NICOUD, F. & POINSOT, T. 2006b Large-eddy simulations of a turbulent flow around a multi-perforated plate. In Complex effects in LES 56, 289–303. 187
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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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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
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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: BIBLIOGRAPHIE HALE, C. A., PLESNIAK
Page 189 and 190: BIBLIOGRAPHIE MOST, A. & BRUEL, P.
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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