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The 22 November 2022 at 14h30

PhD Defense : Soumyo SENGUPTA : “Advanced methods for meshes in High Performance Computing of explosion simulation”

Nathalie BROUSSET |  Conference room - CERFACS - Toulouse |  

Link youtube : https://youtu.be/qKk1Q-MUGDI

Abstract :

Tremendous improvements have been made in numerical simulation using LES (Large Eddy Simulation) over the past thirty years. This was possible with the introduction of more robust numerical methods, improved boundary condition modeling, and more accurate, detailed chemistries in the field of combustion. High-performance computing is a key factor so that these simulations can be performed in a reasonable time frame and use realistic large-scale representative geometries. Even with the advances in all of these mentioned fields, the bottleneck for solving these problems still remains the initial mesh resolution/quality. The focus of this thesis is to first understand why the mesh resolution is important through global stability analysis and then to alleviate this problem by using runtime dynamic mesh adaptation for combustion related explosion problems.

The first part of the manuscript deals with global stability analysis (GSA) of the linear convection-diffusion equation (LCDE) and linear convection-diffusion reaction equation (LCDRE) for non-reacting and reacting flows respectively. This analysis shows the importance of the non-dimensional parameters such as CFL number Nc, Peclet number Pe and Damkohler number, Da on stability, dispersive and diffusive nature of the numerical scheme chosen (Lax-Wendroff and TTGC schemes). Through the analysis, the importance of mesh resolution to obtain an accurate, stable solution for any numerical problem is highlighted. Especially, when solving realistic reacting flow problems, it is of paramount importance to resolve the flame front adequately to obtain accurate solutions. To overcome this issue, when solving realistic large-scale reacting flow simulations it is useful to use run-time dynamic mesh refinement for accuracy and cost benefits.

In the second part of the manuscript, two different dynamic mesh adaptation techniques are explained. Although using a similar generic algorithm, the differences between the two techniques are detailed. Several test cases are simulated to validate the adaptation techniques. An appropriate quantity of interest (QOI) is chosen according to the case studied. Using this quantity of interest, two large-scale, compressible, and turbulent reacting flow test cases are simulated using dynamic mesh adaptation.

Jury :

JENS-D. MUELLER             Queen Mary Univ. of London   Referee

VINCENT MOUREAU          CORIA                                     Referee

ANDREAS KEMPF              Universit¨at Duisburg-Essen    Examiner

NABIHA CHAUMEIX            CNRS ICARE                          Examiner

LAURENT GICQUEL           CERFACS                                Director

GABRIEL STAFFELBACH   CERFACS                                Co-Director


ISAF project : To accelerate the transition to SAFs, SAFRAN and CERFACS have together obtained an allocation of 44 million CPU hours on the LUMI-C super-computer as part of the EuroHPC Regular Access call in November 2022.

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The objective of the ISAF project is to study the impact of SAFs (Sustainable Aviation Fuels) on engine operation and pollutant emissions, using high-fidelity Large Eddy Simulations (LES). The methodology developed at CERFACS combines Analytically Reduced Chemistry (ARC) with a multi-component evaporation model to capture the effect of fuel. The target configurations range from academic burners (CRSB at CORIA, SSB at DLR Stuttgart), to isolated industrial injection systems (MICADO at ONERA, HERON at CORIA) and complete annular combustor configurations (BEARCAT at SAFRAN, NTNU test bench).Read more

A CERFACS article distinguished in Scilight (https://doi.org/10.1063/10.0017474)

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