Abstract
Numerical techniques for multi-species chemical reacting flows are applied to study the macrostructures of oblique detonation waves in confined space. The key features, the evolution of the overall wave structure, and the transitional criteria are analysed. The results show that with the increase of wedge angle, four structures appear in turn: shock-induced combustion, oblique detonation double regular reflection, Mach reflection in reflux zone, and wedge combustion. The simulations reveal three critical conditions of the compression angle for the maintenance of stable wave structures, i.e., lower-critical, sub-critical, and upper critical conditions. In addition, the transition between regular and Mach reflections occurs during the evolution process of the macro wave structure.
Translated title of the contribution | Numerical Study on Structural Evolution and Transitional Criteria of Oblique Detonation Waves in Confined Space |
---|---|
Original language | Chinese (Traditional) |
Pages (from-to) | 738-744 |
Number of pages | 7 |
Journal | Tuijin Jishu/Journal of Propulsion Technology |
Volume | 42 |
Issue number | 4 |
DOIs | |
Publication status | Published - Apr 2021 |
Externally published | Yes |