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.

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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

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article

Numerical Study of the Induction Length Effect on Oblique Detonation Waves

Yu Liu, Shilong Sun, Gaoxiang Xiang
Aerospace
Combustion and Detonation Processes
article

Numerical Study of the Induction Length Effect on Oblique Detonation Waves

Yu Liu, Shilong Sun, Gaoxiang Xiang
article en

Abstract

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.

AerospaceVol. 12(9)
Northwestern Polytechnical University (CN), China Aerodynamics Research and Development Center (CN)
Aerospace Technology Institute, National Natural Science Foundation of China, China Aerodynamics Research and Development Center
Openalex Percentile: Top 68%
Combustion and Detonation Processes
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