High performance parallel computing of flows in complex geometries: II. Applications

Computational Science and Discovery

Volumn 2, Issue 1, 2009, Pages

  Gourdain, N ^a   Gicquel, L ^a   Staffelbach, G ^a   Vermorel, O ^a   Duchaine, F ^a   Boussuge, J F ^a   Poinsot, T ^b  

^a CERFACS   (France)

^b IMFT   (France)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 76149130407     PISSN: 17494680     EISSN: 17494699     Source Type: Journal    
DOI: 10.1088/1749-4699/2/1/015004     Document Type: Article

References (75)

1. Amdahl G 1967 Validity of the single processor approach to achieving large-scale computing capabilities AFIPS Conf. Proc. 30 483-5
2. Arakawa C, Fleig O, Iida M and Shimooka M 2005 Numerical approach for noise reduction of wind turbine blade tip with earth simulator J. Earth Simulator 2 11-33
3. Arts T, Lambert de Rouvroit M and Rutherford A W 1990 Aero-thermal investigation of a highly loaded transonic linear turbine guide vane cascade-a test case for inviscid and viscous flow computations VKI Technical Note 174
4. 2 flames with complex chemistry in two-dimensional turbulent flows J. Fluid Mech. 281 1-32
5. Boileau M, Staffelbach G, Cuenot B, Poinsot T and Bérat C 2008 LES of an ignition sequence in a gas turbine engine J. Combust. Flame 154 2-22
6. Bogey C and Bailly C 2006 Investigation of downstream and sideline subsonic jet noise using large eddy simulations Theor. Comput. Fluid Dyn. 20 23-40
7. Boudier G, Gicquel L, Poinsot T, Bissières D and Berat C 2007 Comparison of LES, RANS and experiments in an aeronautical gas turbine combustion chamber Proc. Comb. Inst. 31 3075-82
8. Boudier G, Gicquel L Y M and Poinsot T 2008 Effects of mesh resolution on large eddy simulation of reacting flows in complex geometry combustors J. Combust. Flame 155 196-214
9. Boudier G, Lamarque N, Staffelbach G, Gicquel L Y M and Poinsot T 2009 Thermo-acoustic stability of a helicopter gas turbine combustor using large eddy simulations Int. J. Aeroacoust. 8 69-94
10. Brunet V and Deck S 2008 Zonal-detached eddy simulation of transonic buffet on a civil aircraft type configuration 46th AIAA Aerospace Science Meeting and Exhibit (Reno, USA)
11. Cambier L and Veuillot J-P 2008 Status of the elsA CFD software for flow simulation and multidisciplinary applications 46th AIAA Aerospace Science Meeting and Exhibit (Reno, USA)
12. Chen J H et al 2009 Terascale direct numerical simulations of turbulent combustion using S3D Comput. Sci. Discov. 2 015001
13. Chen J H, Hawkes E R, Sankaran R, Mason S D and Im H G 2006 Direct numerical simulation of ignition front propagation in a constant volume with temperature inhomogeneities, part I: fundamental analysis and diagnostics J. Combust. Flame 145 128-44
14. Colin O and Rudgyard M 2000 Development of high-order Taylor-Galerkin schemes for unsteady calculations J.Comput. Phys. 162 338-71
15. Deck S 2005 Numerical simulation of transonic buffet over a supercritical airfoil 2005 AIAA J. 43 1556-66
16. Delbove J 2006 Unsteady simulations for flutter prediction Proc. Third Int. Conf. on CFD-ICCFD3 pp 205-10
17. Delville J, Ukeiley L, Cordier L, Bonnet J and Glauser M 1999 Examination of large-scale structures in a turbulent plane mixing layer. Part 1. Proper orthogonal decomposition J. Fluid Mech. 391 92-122
18. Denton J D and Singh U K 1979 Time marching methods for turbomachinery flow calculations (VKI Lecture Series) (Brussels: Von Karman Institute)
19. Domercq O and Escuret J-F 2007 Tip clearance effect on high-pressure compressor stage matching J. Power Energy 221 759-67
20. Duchaine F, Corpron A, Pons L, Moureau V, Nicoud F and Poinsot T 2009 Development and assessment of a coupled strategy for conjugate heat transfer with large eddy simulation. Application to a cooled turbine blade Int. J. Heat Fluid Flow at press (doi: 10.1016/j.ijheatfluidflow.2009.07.004)
21. Février P, Simonin O and Squires K D 2005 Partitioning of particle velocities in gas-solid turbulent flows into a continuous field and a spatially uncorrelated random distribution: theoretical formalism and numerical study J. Fluid Mech. 533 1-46
22. Freund J B 2001 Noise sources in a low-Reynolds number turbulent jet at mach 0.9 J. Fluid Mech. 438 277-305
23. Garcia M 2009 Développement et validation du formalisme Euler-Lagrange dans un solveur parallèle et non-structuré pour la simulation aux grandes échelles PhD thesis University of Toulouse
24. Gicquel L Y M, Staffelbach G, Cuenot B and Poinsot T 2008 Large eddy simulations of turbulent reacting flows in real burners: the status and challenges, SciDAC 2008 J. Phys.: Conf. Ser. 125 17
25. Gökalp I, Chauveau C, Morin C, Vieille B and Birouk M 2000 Improving droplet breakup and vaporisation models, including high pressure and turbulence effects Atomization Sprays 10 475-510
26. Gopinath A, van der Weide E, Alonso J J, Jameson A, Ekici K and Hall K C 2007 Three-dimensional unsteady multi-stage turbomachinery simulations using the harmonic balance technique 45th AIAA Aerospace Sciences Meeting and Exhibit (Reno, USA) paper 2007-0892
27. Gourdain N, Burguburu S, Michon G-J, Ouayahya N, Leboeuf F and Plot S 2006 About the numerical simulation of rotating stall mechanisms in axial compressors ASME Turbo Expo paper GT2006-90223 (Barcelona, Spain)
28. Gourdain N, Ottavy X and Vouillarmet A 2009a Experimental and numerical investigation of unsteady flows in a high-speed three stages compressor 8th European Turbomachinery Conference paper 2009-107 (Graz, Austria)
29. Gourdain N and Leboeuf F 2009b Unsteady simulation of an axial compressor stage with casing and blade passive treatments J. Turbomachinery 130
30. Gourdain N, Gicquel L, Montagnac M, Vermorel O, Gazaix M, Staffelbach G, Garcia M, Boussuge J-F and Poinsot T 2009c High performance computing of complex geometries: I. Methods Comput. Sci. Discov. 2 015003
31. Hall K C, Dowell E H and Thomas J P 2003 Nonlinear reduced order modeling of limit cycle oscillations of aircraft wings and wing/store Technical Report Duke University
32. Hathaway M D, Herrick G, Chen J and Webster R 2004 Time accurate unsteady simulation of the stall inception process in the compression system of a US army helicopter gas turbine engine Proc. DoD Users Group Conf. (Washington, DC, USA) pp 182-93
33. Hathaway M D 2006 Passive endwall treatments for enhancing stability Advances in Axial Compressor Aerodynamics (VKI Lecture Series) (Brussels: Von Karman Institute)
34. He L 1990 An Euler solution for unsteady flows around oscillating blades J. Turbomach. 112 714-22
35. He L 1997 Computational study of rotating-stall inception in axial compressors J. Propulsion Power 13 31-8
36. Homeier L and Haselbach F 2005 Film cooling of highly loaded blades 17th ISABE Conf. paper AIAA-2005-1114 (Munich, Germany)
37. Im H G, Chen J H and Chen J-Y 1999 Chemical response of methane/air diffusion flames to unsteady strain rate J. Combust. Flame 118 204-12
38. James S, Zhu J and Anand M 2006 Large eddy simulations as a design tool for gas turbine combustion systems AIAA J. 44 674-86
39. Jameson A 1991 Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings 10th AIAA Computational Fluid Dynamics Conf. paper 91-1596
40. Lefebvre A H 1999 Gas Turbine Combustion 2nd edn (London: Taylor and Francis)
41. Lignell D O, Chen J H, Smith P J, Lu T and Law C K 2007 The effect of flame structure on soot formation and transport in turbulent nonpremixed flames using direct numerical simulation J. Combust. Flame 151 2-28
42. Liou M S 1996 A sequel to AUSM: AUSM+ J. Comput. Phys. 129 364-82
43. Lumley J L 1978 Computational modelling of turbulent flows Adv. Appl. Mech. 18 123-76
44. Medic G, Kalitzin G, You D, Herrmann M, Ham F, van der Weide E, Pitsch H and Alonso J J 2006 Integrated RANS/LES computations of turbulent flow through a turbofan jet engine Annual Research Briefs (Stanford University)
45. Mendez S and Nicoud F 2008 Large eddy simulation of a bi-periodic turbulent flow with effusion J. Fluid Mech. 598 27-65
46. Miller R S and Bellan J 1999 Direct numerical simulation of a confined three-dimensional gas mixing layer with one evaporating hydrocarbon-droplet laden stream J. Fluid Mech. 384 293-338
47. Mizobuchi Y, Shinjo J, Ogawa S and Takeno T 2005 A numerical study on the formation of diffusion flame islands in a turbulent hydrogen jet lifted flame Proc. Combust. Inst. 30 611-9
48. Moin P and Apte S 2006 Large eddy simulation of realistic turbine combustors AIAA J. 44 698-708
49. Nybelen L and Deniau H 2009 Spatial simulation of a co-rotating vortex merging process in unstable conditions (FAR-Wake workshop, Marseille, France, 2008) Int. J. Methods in Fluids 61 23-56
50. Ottavy X, Trébinjac I, Vouillarmet A and Arnaud D 2003 Laser measurements in high speed compressors for rotor-stator interaction analysis Proc. ISAIF 6th, Shanghai, April 2003
51. Poinsot T and Veynante D 2005 Theoretical and Numerical Combustion 2nd edn (R T Edwards)
52. Reveillon J and Vervisch L 2000 Accounting for spray vaporization in non-premixed turbulent combustion modeling: a single droplet model J. Combust. Flame 121 75-90
53. Rossow C and Kroll N 2008 High performance computing serves aerospace engineering: opportunities for next generation product development 46th AIAA Aerospace Science Meeting and Exhibit (Reno, USA)
54. Schluter J, Apte S, Kalitzin G and van der Weide E 2005 Large-scale integrated LES-RANS simulations of a gas turbine engine Annual Research Briefs (: Stanford University)
55. Seiser R, Frank J H, Liu S, Chen J H, Sigurdsson R J and Seshadri K 2005 Ignition of Hydrogen in unsteady nonpremixed flows Proc. Combust. Inst. 30 423-30
56. Sicot F, Puigt G and Montagnac M 2008 Block-Jacobi implicit algorithms for the time spectral method AIAA J. 46 3080-89
57. Sieverding C H, Richard H and Desse J-M 2003 Turbine blade trailing edge flow characteristics at high subsonic outlet mach number J. Turbomachin. 125 298-309
58. Smagorinsky J S 1963 General circulation experiments with the primitive equations: I. the basic experiment Mon. Weather Rev. 91 99-163
59. Smith C, Beratlis N, Squires K, Balaras E and Tsunoda M 2008 Direct numerical simulations of the flow around a golf ball: effect of rotation 61st Annual Meeting of the APS Division of Fluid Dynamics (San Antonio, USA)
60. Soufiani A and Djavdan E 1994 A comparison between weighted sum of gray gases and statistical narrow-band radiation models for combustion applications J. Combust. Flame 97 240-50
61. Spalart P R and Allmaras S R 1992 A one equation turbulence model for aerodynamic flows AIAA paper 92-0439
62. Spalart P R, Jou W-H, Stretlets M and Allmaras S R 1997 Comments on the feasibility of LES for wings and on the hybrid RANS/LES approach, advances in DNS/LES Proc. First AFOSR Int. Conf. on DNS/LES
63. Staffelbach G, Gicquel L Y M, Boudier G and Poinsot T 2009 Large eddy simulation of self excited azimuthal modes in annular combustors Proc. Combustion Institute (Pittsburgh, USA) vol 32
64. Tennekes H and Lumley J L 1972 A First Course in Turbulence (Cambridge, MA: MIT Press)
65. Truffin K and Poinsot T 2005 Comparison and extension of methods for acoustic identification of burners J. Comb. Flame 142 388-400
66. van der Weide E, Kalitzin G, Schluter J and Alonso J J 2006 Unsteady turbomachinery computations using massively parallel platforms 44th AIAA Aerospace Sciences Meeting and Exhibit (Reno, USA)
67. van der Weide E, Mattson K, Svärd M, Nordström J and Gong J 2008 Recent developments of the SBP/SAT discretization technique on multi-block structured grids Thermal and Fluid Sciences Affiliates Program, Stanford
68. van Leer B 1979 Towards the ultimate conservative difference scheme, V: a second order sequel to Godunov's method J. Comput. Phys. 32 101-36
69. Varga C, Lasheras J and Hopfinger E 2003 Initial breakup of a small-diameter liquid jet by a high-speed gas stream J. Fluid Mech. 497 405-34
70. Vermorel O, Bédat B, Simonin O and Poinsot T 2003 Numerical study and modelling of turbulence modulation in a particle laden slab flow J. Turbul. 4 025
71. Weber D P, Wei T Y C, Brewster R A and Rock D T 2000 High fidelity thermal-hydraulic analysis using CFD and massively parallel computers 4th Int. Conf. Supercomputing in Nuclear Applications (Tokyo, Japan)
72. Wilcox D C 1988 Reassessment of the scale-determining equation for advanced turbulence models AIAA J. 26 1299-310
73. Wu Y, Haworth D C, Modest M F and Cuenot B 2005 Direct numerical simulation of turbulence/radiation interaction in premixed combustion systems Proc. Combust. Inst. 30 639-46
74. Yang H, Nuernberger D and Kersken H-P 2005 Towards excellence in turbomachinery CFD: a hybrid structured-unstructured RANS solver J. Turbomachinery 128 390-402
75. Yoon S and Jameson A 1987 An LU-SSOR scheme for the euler and Navier-Stokes equations 25th AIAA Aerospace Sciences Meeting (Reno, USA) paper 87-0600