Abstract
Two-dimensional numerical simulations are conducted based on the Eulerian-Lagrangian method to model a gaseous detonation laden with monodispersed water droplets. The premixed mixture is a slightly diluted stoichiometric hydrogen oxygen mixture at low pressure. The outcome of the interactions of the droplet breakup with the cellular instabilities and the non-uniform flow behind the leading front is analyzed. The simulation results are also analyzed using instantaneous flow fields and Favre average profiles for water droplets. Breakup occurs mainly near the detonation front. The mean final diameter of the water droplets at the end of the breakup process is the same regardless of the initial strength of the leading shock or whether it is lower or greater than the Chapman-Jouguet value. The polydispersity comes from local phenomena behind the leading shock, such as forward jets coming from triple point collisions, transverse waves and a combination of both. The total breakup time is longer than that estimated from post-shock conditions and the present finding is in line with the previous experimental results on spray detonation.
Original language | English |
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Pages (from-to) | 3709-3716 |
Number of pages | 8 |
Journal | Proceedings of the Combustion Institute |
Volume | 38 |
Issue number | 3 |
DOIs | |
Publication status | Published - 2021 |
Event | 38th International Symposium on Combustion, 2021 - Adelaide, Australia Duration: 2021 Jan 24 → 2021 Jan 29 |
Keywords
- Breakup
- Gaseous detonation
- Polydispersity
- Water spray
ASJC Scopus subject areas
- Chemical Engineering(all)
- Mechanical Engineering
- Physical and Theoretical Chemistry