Numerical study of oblique detonation initiations with chain branching kinetics

Honghui Teng, Pengfei Yang, Zonglin Jiang

科研成果: 书/报告/会议事项章节会议稿件同行评审

6 引用 (Scopus)

摘要

Oblique detonations induced by semi-infinite wedge are simulated by solving Euler equations with chain branching kinetics. Numerical results show the initiation can be triggered by either the abrupt transition or smooth transition, dependent on incident Ma Min and wedge angle θ, and then their effects on the oblique detonation angle β and initiation length Lini are analyzed. When θ increases, Lini decreases monotonically but β has a minimum value, corresponding to θ = 29° in this study. When Min decreases, both Lini and β increases monotonically until Min decreases below certain critical value, Min = 9.2 in this study. Then low inflow Ma effects generate the maximum Lini, with the complex of ODW (oblique detonation wave), SODW (secondary oblique detonation wave) and SIDW (self-ignition deflagration wave). The transient process is observed, demonstrating the structure can self-adjust to find a proper position. The wave structure suggests two wave/heat release process determining the detonation initiation. In the cases with high Min featured by SIDW, the oblique-shock induced self-ignition dominates, and Lini increases when Min decreases. In the cases with low Min featured by SODW, the interaction of ODW and SODW dominates, and Lini decreases when Min decreases.

源语言英语
主期刊名AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting
出版商American Institute of Aeronautics and Astronautics Inc.
ISBN(电子版)9781624104473
DOI
出版状态已出版 - 2017
已对外发布
活动55th AIAA Aerospace Sciences Meeting - Grapevine, 美国
期限: 9 1月 201713 1月 2017

出版系列

姓名AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting

会议

会议55th AIAA Aerospace Sciences Meeting
国家/地区美国
Grapevine
时期9/01/1713/01/17

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