Abstract
The unsteady reflection of detonation waves over cylindrical convex surfaces is numerically investigated using a high-resolution adaptive mesh refinement technique combined with a detailed reaction mechanism. Results reveal that cellular instabilities complicate the determination of the transition point from regular reflection to Mach reflection. However, the triple-point trajectories connecting the incident detonation wave and Mach stem remain largely unaffected by these instabilities. This consistency is confirmed by reducing the radius and the initial angle of the cylindrical surfaces. Finally, no universal scaling is observed across all configurations. At larger radii, the triple-point trajectories tend to stay closer to the surface.
| Original language | English |
|---|---|
| Article number | 081705 |
| Journal | Physics of Fluids |
| Volume | 37 |
| Issue number | 8 |
| DOIs | |
| Publication status | Published - 21 Aug 2025 |
Keywords
- NUMERICAL-SIMULATION
- Mach reflection
ASJC Scopus subject areas
- Computational Mechanics
- Condensed Matter Physics
- Mechanics of Materials
- Mechanical Engineering
- Fluid Flow and Transfer Processes
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