This work is part of the development of a new generation CFD solver, Argo, based on the discontinuous Galerkin Method (DGM), specifically targeted towards accurate, adaptive, reliable and fast DNS and LES of industrial aerodynamic flows. Several aspects were investigated in IDIHOM. A first activity was the optimisation of the parallellisation strategy, resulting in highly efficient scaling, demonstrated on some of the largest computers in Europe. A second activity concerned the assessment and validation on several academic benchmark problems of the capability of DGM to perform direct numerical simulation (DNS) and (implicit) Large Eddy Simulation (iLES). Two moderately complex flows are treated, namely the ILES of the transitional flow in t...
Cette thèse vise à développer et évaluer la méthode de Galerkin discontinue (DG) pour la simulationd...
The turbulent flow over the DrivAer fastback model is here investigated with an orderadaptive discon...
To enhance prediction capacities and therefore allow more advanced aeronautic and aero-propulsive de...
Due to the continuously increasing economical and environmental constraints, the standard industrial...
peer reviewedThis work is part of the development of a new generation of CFD solvers on the basis of...
peer reviewedThis paper concerns implicit large eddy simulation (ILES) of turbulent flows of industr...
peer reviewedAn implicit time integration, high-order discontinuous Galerkin method is assessed on t...
The recent advent of unstructured high order methods holds the promise of transforming industrial co...
There is a continued need to further capabilities of turbomachinery flow design and analysis method ...
In recent years Discontinuous Galerkin (DG) methods have emerged as one of the most promising high-o...
Computational Fluid Dynamics (CFD) is a useful tool that enables highly cost-effective numerical sol...
We present a performance analysis of the numerical code DG-comp which is based on a Local Discontinu...
peer reviewedHigh pressure turbine (HPT) blades are cooled partly by guiding air from the compressor...
In recent years Computational Fluid Dynamics (CFD) has become a widespread practice in industry. The...
This paper presents the second validation step of a compressible discontinuous Galerkin solver with ...
Cette thèse vise à développer et évaluer la méthode de Galerkin discontinue (DG) pour la simulationd...
The turbulent flow over the DrivAer fastback model is here investigated with an orderadaptive discon...
To enhance prediction capacities and therefore allow more advanced aeronautic and aero-propulsive de...
Due to the continuously increasing economical and environmental constraints, the standard industrial...
peer reviewedThis work is part of the development of a new generation of CFD solvers on the basis of...
peer reviewedThis paper concerns implicit large eddy simulation (ILES) of turbulent flows of industr...
peer reviewedAn implicit time integration, high-order discontinuous Galerkin method is assessed on t...
The recent advent of unstructured high order methods holds the promise of transforming industrial co...
There is a continued need to further capabilities of turbomachinery flow design and analysis method ...
In recent years Discontinuous Galerkin (DG) methods have emerged as one of the most promising high-o...
Computational Fluid Dynamics (CFD) is a useful tool that enables highly cost-effective numerical sol...
We present a performance analysis of the numerical code DG-comp which is based on a Local Discontinu...
peer reviewedHigh pressure turbine (HPT) blades are cooled partly by guiding air from the compressor...
In recent years Computational Fluid Dynamics (CFD) has become a widespread practice in industry. The...
This paper presents the second validation step of a compressible discontinuous Galerkin solver with ...
Cette thèse vise à développer et évaluer la méthode de Galerkin discontinue (DG) pour la simulationd...
The turbulent flow over the DrivAer fastback model is here investigated with an orderadaptive discon...
To enhance prediction capacities and therefore allow more advanced aeronautic and aero-propulsive de...