Numerical Study of the Induction Length Effect on Oblique Detonation Waves
The typical structure of an oblique detonation wave (ODW) consists of a leading shock wave followed by a coupled shock-flame complex. The distance from the leading shock’s originating point to the ignition onset is referred to as the induction length. This work numerically studies the induction length effect using a two-step induction-reaction kinetic model. Results reveal that the induction length governs the transition pattern of ODWs. By testing four distinct induction lengths, four ODW regimes are identified, including a prompt ODW, a delayed smooth ODW, a delayed abrupt ODW, and a delayed abrupt ODW with an upstream triple point in oscillatory motion. The mechanisms behind these regimes are analyzed in detail. Additionally, hysteresis is observed when the induction length decreases from a larger value, demonstrating that this phenomenon can be influenced by the kinetic process.
Authors
- Yu Liu (ORCID: https://orcid.org/0000-0002-3327-7175)
- Shilong Sun (ORCID: https://orcid.org/0009-0002-8393-6551)
- Gaoxiang Xiang (ORCID: https://orcid.org/0000-0002-6214-1234)
Institutions
- Northwestern Polytechnical University (CN)
- China Aerodynamics Research and Development Center (CN)
Publication Details
- Journal
- Aerospace
- Published
- 2025-09-01
- DOI
- https://doi.org/10.3390/aerospace12090792
- Primary Topic
- Combustion and Detonation Processes
- Type
- article
- Field-Weighted Citation Impact
- 0.00
Funders
- Aerospace Technology Institute
- National Natural Science Foundation of China
- China Aerodynamics Research and Development Center