Abstract
An Eulerian Monte-Carlo approach, the so-called Eulerian stochastic fields (ESF) method is implemented and evaluated for simulation of non-premixed hydrogen/air combustion in supersonic flows. The ESF method is integrated into a compressible flow large eddy simulation (LES) solver, and validated on a supersonic combustor with a strut as flame-holder. Comparison with experimental data and with results from a well-stirred reactor (WSR) model demonstrates the advantage of the LES-ESF method for simulation of local-extinction and re-ignition phenomena. The hydrogen/air flame structure and the stabilization of the combustion process in the supersonic combustor are analysed based on the present LES-ESF method. Oscillation of the recirculation zones is found to be the dominant mechanism for the local-extinction/re-ignition and the flame stabilization under the present condition.
Original language | English |
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Pages (from-to) | 1264-1275 |
Number of pages | 12 |
Journal | International Journal of Hydrogen Energy |
Volume | 42 |
Issue number | 2 |
Early online date | 2 Oct 2016 |
DOIs | |
Publication status | Published - 12 Jan 2017 |
Keywords
- Eulerian stochastic fields
- Large eddy simulation
- Local-extinction
- Re-ignition
- Supersonic
- Transported probability density function
ASJC Scopus subject areas
- Renewable Energy, Sustainability and the Environment
- Fuel Technology
- Condensed Matter Physics
- Energy Engineering and Power Technology