The University of Southampton
University of Southampton Institutional Repository

Parallel adaptive simulation of rotating detonation engines

Parallel adaptive simulation of rotating detonation engines
Parallel adaptive simulation of rotating detonation engines
The rotating detonation engine is a promising realization of pressure gain combustion for propulsion and power generation systems. A rotating detonation engine running on ethylene-oxygen is simulated by using AMROC with a second-order accurate finite volume method and approximate Riemann solvers. Multi-step chemical kinetic mechanisms are employed with a splitting approach. The rotating detonation is studied in a 2-D unwrapped chamber with premixed and non-premixed injections and is then simulated in a 3-D annular chamber. The results show that using the adaptive mesh refinement method can simulate rotating detonation problems efficiently.
rotating detonation engine, reactive flow simulation, adaptive mesh refinement, adaptive curvilinear mesh, parallelization
Civil-Comp Press
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 (2023) Parallel adaptive simulation of rotating detonation engines. In Proc. of 11th Int. Conf. on Engineering Computational Technology - ECT2022. vol. CCC 2, Civil-Comp Press. 6 pp . (doi:10.4203/ccc.2.1.3).

Record type: Conference or Workshop Item (Paper)

Abstract

The rotating detonation engine is a promising realization of pressure gain combustion for propulsion and power generation systems. A rotating detonation engine running on ethylene-oxygen is simulated by using AMROC with a second-order accurate finite volume method and approximate Riemann solvers. Multi-step chemical kinetic mechanisms are employed with a splitting approach. The rotating detonation is studied in a 2-D unwrapped chamber with premixed and non-premixed injections and is then simulated in a 3-D annular chamber. The results show that using the adaptive mesh refinement method can simulate rotating detonation problems efficiently.

Text
ctr_peng_deiterding_0602 - Accepted Manuscript
Download (300kB)

More information

Accepted/In Press date: 23 August 2022
Published date: 15 June 2023
Venue - Dates: 11th International Conference on Engineering Computational Technology, , Montpellier, France, 2022-08-23 - 2022-08-25
Keywords: rotating detonation engine, reactive flow simulation, adaptive mesh refinement, adaptive curvilinear mesh, parallelization

Identifiers

Local EPrints ID: 470589
URI: http://eprints.soton.ac.uk/id/eprint/470589
PURE UUID: 085ce706-755e-4e49-9c69-9125c1669814
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: 14 Oct 2022 16:32
Last modified: 13 Jun 2024 01:57

Export record

Altmetrics

Download statistics

Downloads from ePrints over the past year. Other digital versions may also be available to download e.g. from the publisher's website.

View more statistics

Atom RSS 1.0 RSS 2.0

Contact ePrints Soton: eprints@soton.ac.uk

ePrints Soton supports OAI 2.0 with a base URL of http://eprints.soton.ac.uk/cgi/oai2

This repository has been built using EPrints software, developed at the University of Southampton, but available to everyone to use.

We use cookies to ensure that we give you the best experience on our website. If you continue without changing your settings, we will assume that you are happy to receive cookies on the University of Southampton website.

×