Adaptive mesh refinement based simulations of three-dimensional detonation combustion in supersonic combustible mixtures with a detailed reaction model
- Submitting institution
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University of Southampton
- Unit of assessment
- 12 - Engineering
- Output identifier
- 19514519
- Type
- D - Journal article
- DOI
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10.1016/j.ijhydene.2015.11.093
- Title of journal
- International Journal of Hydrogen Energy
- Article number
- -
- First page
- 3222
- Volume
- 41
- Issue
- 4
- ISSN
- 0360-3199
- Open access status
- Out of scope for open access requirements
- Month of publication
- December
- Year of publication
- 2015
- URL
-
-
- Supplementary information
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- Request cross-referral to
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- Output has been delayed by COVID-19
- No
- COVID-19 affected output statement
- -
- Forensic science
- No
- Criminology
- No
- Interdisciplinary
- No
- Number of additional authors
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4
- Research group(s)
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-
- Proposed double-weighted
- No
- Reserve for an output with double weighting
- No
- Additional information
- Employing detonation combustion in jet and rocket engines will increase their efficiency by at least 15%. This paper presents one of the first 3D simulations of detonation initiation in a realistic system with full-scale hydrogen-oxygen kinetics. Utilising the AMROC solver on the Tianhe-2 supercomputer, this work was enabled by international collaboration. This paper lead to R.Deiterding being invited to give the plenary lecture at the International Symposium of Combustion Instabilities in 01/2017 in Beijing. The herein demonstrated unique solver capabilities were key to R.Deiterding being invited to EPSRC programme grant EP/P000878/1, with £512,549 allocated to AMROC development for high-enthalpy flows.
- Author contribution statement
- -
- Non-English
- No
- English abstract
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