Abstract
The unstable behavior of the detonation is an important issue in predicting detonation limits and safety problems. The present study aims to obtain information of the unstable behavior near the detonation propagating limit in methane/oxygen gas mixture for various initial pressures and tube diameters. The detonation velocity rapidly decreases near α = 1.0 and deviates from the theoretical value for α < 1.0 conditions (α = πd/λ; d: tube diameter; λ: cell width). The onset of the single-head spinning is α = 1.0. For α < 1.0 conditions, the transition to the single-head spinning from small cells and the failure of cellular patterns were observed. For α > 1.0 conditions, the propagation mode was unstable. The unstable phenomenon means that the cellular pattern repeats multi-head and single-head spinning in turn.
Original language | English |
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Pages (from-to) | 2012-2025 |
Number of pages | 14 |
Journal | Combustion science and technology |
Volume | 188 |
Issue number | 11-12 |
DOIs | |
Publication status | Published - 2016 Dec 1 |
Externally published | Yes |
Keywords
- CH/O
- Detonation
- Experiment
- Propagating limit
- Unstable
ASJC Scopus subject areas
- Chemistry(all)
- Chemical Engineering(all)
- Fuel Technology
- Energy Engineering and Power Technology
- Physics and Astronomy(all)