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Turbulent flows |
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Heated square cylinders in tandem in a cold flow: isosurface of Q criterion colored by the temperature
Date: 2009
Author(s): Florent Duchaine and Matthieu Boileau
Codes used: AVBP
Credit: CERFACS, AIRBUS
Reference: pdf to be putted
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Instantaneous turbulent field around a high pressure turbine blade.
Date: 2010
Author(s): Elena Collado and Florent Duchaine
Codes used: AVBP
Credit: CERFACS
Reference: pdf
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Laminar to turbulent boundary layer on the Spalart and Strelets configuration (Mechanisms of transition and heat transfer in a separation bubble. JFM 2000).
Date: 2012
Author(s): Florent Duchaine
Codes used: AVBP
Credit: CERFACS
Reference: pdf to be putted
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Laminar to turbulent boundary layer on the succion side of a low pressure turbine blade.
Date: 2012
Author(s): Florent Duchaine
Codes used: AVBP
Credit: CERFACS
Reference: pdf to be putted
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Code coupling for Multi-physics |
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Determination of an industrial combustor wall temperature
Date: 2006
Author(s): Florent Duchaine and Eric Mercier
Codes used: N3S-Natur, ASTRE, Abaqus
Credit: CERFACS, SNECMA
Reference: pdf
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Determination of multiperforation wall temperature in a 2D case
Date: 2008
Author(s): Florent Duchaine
Codes used: AVBP, AVTP
Credit: CERFACS
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Determination of multiperforation wall temperature in a 3D case
Date: 2008
Author(s): Florent Duchaine
Codes used: AVBP, AVTP
Credit: CERFACS
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Conjugate heat transfer in the Nasa C3X blade
Date: 2008
Author(s): Florent Duchaine
Codes used: AVBP, AVTP
Credit: CERFACS
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Conjugate heat transfer in the T120D blade (European Project AITEB2)
Date: 2008
Author(s): Florent Duchaine
Codes used: AVBP, AVTP
Credit: CERFACS, TURBOMECA
Reference: pdf
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3D Simulation of Coupled Fluid Flow and Solid Heat Conduction for the Calculation of Blade Wall Temperature in a Turbine Stage
Date: 2009
Author(s): Fabien Wlassow and Florent Duchaine
Codes used: elsA, AVTP
Credit: CERFACS, TURBOMECA
Reference: pdf
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Determination of flame holder temperature in an accademic configuration
Date: 2010
Author(s): Florent Duchaine
Codes used: AVBP, AVTP
Credit: Institut de MÈcanique des Fluides de Toulouse
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Determination of heat loads in an industrial combustion chamber by the coupling of reactive fluid dynamcis, radiation and conduction
Date: 2010
Author(s): Jorge Amaya
Codes used: AVBP, PRISSMA, AVTP
Credit: CERFACS, TURBOMECA
Reference: pdf
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Coupled convection, conduction and radiation simulations in an industrial combustion chamber with a vaporizer injector
Date: 2010
Author(s): Jorge Amaya
Codes used: AVBP, PRISSMA, AVTP
Credit: CERFACS, TURBOMECA
Reference: pdf
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Conjugate heat transfer of a hot jet in cross-flow over cold plate
Date: 2010
Author(s): Yannick Hallez
Codes used: AVBP, AVTP
Credit: CERFACS
Reference: pdf
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Conjugate heat transfer in a higly loaded low pressure turbine blade (European Project AITEB2)
Date: 2012
Author(s): Florent Duchaine
Codes used: YALES2, AVTP
Credit: CERFACS
Reference: pdf to be putted
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Conjugate heat transfer of a multiperforated plate with 6 rows
Date: 2012
Author(s): Juan Luis Florenciano and Florent Duchaine
Codes used: AVBP, AVTP
Credit: TURBOMECA - CERFACS
Reference: pdf to be putted
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Code coupling for Multi-components |
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Coupled simulation between LES and RANS for a turbulent tube
Date: 2012
Author(s): Elena Collado and Florent Duchaine
Codes used: AVBP and elsA
Credit: TURBOMECA, CERFACS
Reference: pdf
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Flow past a rotation cylinder with a coupled simulation between two instances of a LES solver (AVBP): one fix to represent the far field and one rotating around the cylinder.
Date: 2012
Author(s): Gaofeng Wang and Florent Duchaine
Codes used: TurboAVBP
Credit: CERFACS
Reference: COFFECI Project: Couplage Fluide/Fluide entre Codes Instationnaires
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Flow in a high pressure turbine stage with a coupled simulation between two instances of a LES solver (AVBP): one fix to represent stator one rotating for the rotor.
Date: 2012
Author(s): Gaofeng Wang and Florent Duchaine
Codes used: TurboAVBP
Credit: CERFACS
Reference: COFFECI Project: Couplage Fluide/Fluide entre Codes Instationnaires
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Flow in a high pressure turbine stage with a coupled simulation between two instances of a LES solver (AVBP): one fix to represent stator one rotating for the rotor.
Date: 2013
Author(s): Gaofeng Wang and Dimitrios Papadogiannis
Codes used: TurboAVBP
Credit: CERFACS
Reference: ASME Turbo EXPO 2013
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Flow in a high pressure turbine stage with a coupled simulation between two instances of a LES solver (AVBP): one fix to represent stator one rotating for the rotor.
Date: 2013
Author(s): Gaofeng Wang and Dimitrios Papadogiannis
Codes used: TurboAVBP
Credit: CERFACS
Reference: ASME Turbo EXPO 2013
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Code assembling |
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Multiobjective shape optimization of a combustion chamber
Date: 2007
Author(s): Florent Duchaine
Codes used: N3S-Natur
Credit: CERFACS, TURBOMECA
Reference: pdf
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