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A three-dimensional solver for simulating reactive flow on curvilinear parallel adaptive meshes

A three-dimensional solver for simulating reactive flow on curvilinear parallel adaptive meshes
A three-dimensional solver for simulating reactive flow on curvilinear parallel adaptive meshes
A generic solver in a parallel Cartesian adaptive mesh refinement framework is extended to simulate reactive flows on structured curvilinear meshes. A second-order accurate finite volume method is used with a grid-aligned Riemann solver for inviscid thermally perfect gas mixtures. Detailed, multi-step chemical kinetic mechanisms are employed with a splitting approach. The prolongation and restriction operators are modified to implement the adaptive mesh refinement algorithm on a mapped mesh. The developed solver is verified with a multispecies shock tube problem and is then used to simulate rotating detonation waves in an annular combustion chamber. The results show that the new solver can simulate high-speed reactive flows efficiently.
Parallel adaptive mesh refinement, Mapped meshes, Reactive flow simulation, Detonation simulation
Peng, Han
62906b46-9628-43fc-921d-b6257b1fec6f
Deiterding, Ralf
ce02244b-6651-47e3-8325-2c0a0c9c6314
Peng, Han
62906b46-9628-43fc-921d-b6257b1fec6f
Deiterding, Ralf
ce02244b-6651-47e3-8325-2c0a0c9c6314

Peng, Han and Deiterding, Ralf (2022) A three-dimensional solver for simulating reactive flow on curvilinear parallel adaptive meshes. In Proc. 33rd Parallel CFD Int. Conf.

Record type: Conference or Workshop Item (Paper)

Abstract

A generic solver in a parallel Cartesian adaptive mesh refinement framework is extended to simulate reactive flows on structured curvilinear meshes. A second-order accurate finite volume method is used with a grid-aligned Riemann solver for inviscid thermally perfect gas mixtures. Detailed, multi-step chemical kinetic mechanisms are employed with a splitting approach. The prolongation and restriction operators are modified to implement the adaptive mesh refinement algorithm on a mapped mesh. The developed solver is verified with a multispecies shock tube problem and is then used to simulate rotating detonation waves in an annular combustion chamber. The results show that the new solver can simulate high-speed reactive flows efficiently.

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More information

Published date: 25 May 2022
Venue - Dates: 33rd Parallel CFD International Conference, , Alba, Italy, 2022-05-25 - 2022-05-27
Keywords: Parallel adaptive mesh refinement, Mapped meshes, Reactive flow simulation, Detonation simulation

Identifiers

Local EPrints ID: 458024
URI: http://eprints.soton.ac.uk/id/eprint/458024
PURE UUID: 9f3ee418-d8b8-4e9a-9337-3e415f465309
ORCID for Han Peng: ORCID iD orcid.org/0000-0003-4503-360X
ORCID for Ralf Deiterding: ORCID iD orcid.org/0000-0003-4776-8183

Catalogue record

Date deposited: 24 Jun 2022 21:52
Last modified: 25 Jun 2022 02:00

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