Abstract
This study aims to systematically characterize the effect of CO/H2 molar ratio on the detonation initiation characteristics of syngas/air mixtures, identify the critical initiation threshold, and provide fuel optimization guidance for pulse detonation engines (PDEs), where short-distance/short-time detonation initiation is a core technical bottleneck. Numerical simulations were performed for 10 cases with CO/H2 ratios ranging from pure CO to pure H2 in a physical model simulating the detonation chamber of PDE, under consistent initial conditions (T=300K, p=1atm) and identical hot jet ignition parameters. The results showed that pure CO could not achieve direct detonation, while the addition of H2 significantly enhanced the detonation sensitivity of the mixture, and the critical CO/H2 molar ratio for successful detonation initiation lay in the range of 1.5 to 2. Three distinct detonation initiation modes were identified, and initiation time/distance showed non-monotonic variation with H2 content. Detonation temperature and velocity decreased monotonically with falling H2 proportion, while detonation pressure increased significantly at CO/H2 ratios above 1:1.5. This study provides quantitative criteria for syngas composition optimization, facilitating the application of clean fuels and promoting the engineering implementation of PDEs.
| Original language | English |
|---|---|
| Article number | 112288 |
| Journal | Aerospace Science and Technology |
| Volume | 177 |
| DOIs | |
| State | Published - Oct 2026 |
Keywords
- Detonation initiation characteristics
- Numerical simulation
- Pulse detonation engine
- Sustainable aviation fuel
- Syngas
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