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Conjugate heat transfer coupling relying on large eddy simulation with complex geometries in massively parallel environments

Jauré, Stéphan. Conjugate heat transfer coupling relying on large eddy simulation with complex geometries in massively parallel environments. PhD, Dynamique des fluides, Institut National Polytechnique de Toulouse, 2012

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Progress in scientific computing has led to major advances in simulation and understanding of the different physical phenomena that exist in industrial gas turbines. However' most of these advances have focused on solving one problem at a time. Indeed' the combustion problem is solved independently from the thermal or radiation problems' etc... In reality all these problems interact: one speaks of coupled problems. Thus performing coupled computations can improve the quality of simulations and provide gas turbines engineers with new design tools. Recently' solutions have been developed to handle multiple physics simultaneously using generic solvers. However' due to their genericity these solutions reveal to be ineffective on expensive problems such as Large Eddy Simulation (LES). Another solution is to perform code coupling: specialized codes are connected together' one for each problem and they exchange data periodically. In this thesis a conjugate heat transfer problem is considered. A fluid domain solved by a combustion LES solver is coupled with a solid domain in which the conduction problem is solved. Implementing this coupled problem raises multiple issues which are addressed in this thesis. Firstly' the specific problem of coupling an LES solver to a conduction solver is considered: the impact of the inter-solver exchange frequency on convergence' possible temporal aliasing' and stability of the coupled system is studied. Then interpolation and geometrical issues are addressed: a conservative interpolation method is developed and compared to other methods. These methods are then applied to an industrial configuration' highlighting the problems and solutions specific to complex geometry. Finally' high performance computing (HPC) is considered: an efficient method to perform data exchange and interpolation between parallel codes is developed. This work has been applied to an aeronautical combustion chamber configuration.

Item Type:PhD Thesis
Uncontrolled Keywords:
Institution:Université de Toulouse > Institut National Polytechnique de Toulouse - INPT (FRANCE)
Laboratory name:
Research Director:
Gicquel, Laurent Y.M. and Duchaine, Florent
Deposited By: Elise Gay Leboul
Deposited On:04 Oct 2017 12:44

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