An Immersed Boundary Method for pressure-based compressible solvers with applications to free-convection flows, acoustic wave propagation and thermal plasma
Immersed Boundary Methods (IBM) are a practical class of methods that enable fluid computations in complex geometry while keeping a structured mesh. Most of the existing IBM have been developed in the framework of incompressible solvers, despite their significant interest to perform simulations in more complex configurations requiring a compressible solver. In the last years, pressure-based solvers met a growing interest to perform numerical simulations of compressible flows, due to their attractive features, as removing the stability condition on the acoustic time step, and being asymptotically preserving of the incompressible regime when the Mach number tends to zero. As this class of compressible solvers share many common features with classical projection methods for incompressible flows, our objective in this paper is to present an adaptation of an efficient and accurate IBM developed for an incompressible solver by Ng et al. in [1] to a pressure-based compressible solver recently published by Urbano et al. in [2] . The proposed algorithm benefits of the attractive properties of the original IBM proposed in [1] while being able to undertake simulations in much more complex configurations. In particular, we will present validations and illustrations of the proposed solver in various configurations as free-convection flows, acoustic waves propagating in a variable section pipe or interacting with a solid obstacle, as well as the description of a thermal plasma during an electric arc discharge in a gas. • A Immersed boundary for a compressible pressure based solver is proposed. • Many original benchmarks involving free. • convection and acoustic wave propagation are presented. • The compressible solver is coupled to a thermal plasma solver. • Preliminary results of an electric arc discharge between electrodes are presented.
Authors
- Pierre Freton (ORCID: https://orcid.org/0000-0002-2491-5841)
- Sébastien Tanguy (ORCID: https://orcid.org/0000-0002-5208-3202)
- Sergiu Coseru (ORCID: https://orcid.org/0000-0002-1771-067X)
- Marie Bibal (ORCID: https://orcid.org/0000-0001-5517-5025)
- Gauthier Bourdon
- Annafederica Urbano (ORCID: https://orcid.org/0000-0002-7576-8685)
- Jean‐Jacques Gonzalez (ORCID: https://orcid.org/0000-0001-6288-3898)
Institutions
- École Nationale de l’Aviation Civile (FR)
- Centre National de la Recherche Scientifique (FR)
- Université Toulouse III - Paul Sabatier (FR)
- Université Fédérale de Toulouse Midi-Pyrénées (FR)
- Institut Superieur de l'Aeronautique et de l'Espace (ISAE-SUPAERO) (FR)
- Institut National Polytechnique de Toulouse (FR)
- Office National d'Études et de Recherches Aérospatiales (FR)
- Institut de Mécanique des Fluides de Toulouse (FR)
- Laboratoire Plasma et Conversion d'Energie (FR)
- École Nationale Supérieure d'Électrotechnique, d'Électronique, d'Informatique, d'Hydraulique et des Télécommunications (FR)
Publication Details
- Journal
- Journal of Computational Physics
- Published
- 2025-01-09
- DOI
- https://doi.org/10.1016/j.jcp.2024.113714
- Citations
- 2
- Primary Topic
- Lattice Boltzmann Simulation Studies
- Type
- article
- Field-Weighted Citation Impact
- 2.67
Funders
- Bpifrance
- Région Occitanie Pyrénées-Méditerranée
- Agence de l'innovation de Défense
- Framatome