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Effects and mechanisms of strut injection strategy on mixing and combustion in oblique detonation engines

Yiming Zhu Yunpeng Qin Dequan Xu Shaohua Zhu Jian An Xianggeng Wei Fei Qin

防务技术2026，Vol.58Issue(4)：53-68,16.

防务技术2026，Vol.58Issue(4)：53-68,16.DOI:10.1016/j.dt.2025.12.022

Effects and mechanisms of strut injection strategy on mixing and combustion in oblique detonation engines

Yiming Zhu ¹Yunpeng Qin ²Dequan Xu ¹Shaohua Zhu ¹Jian An ¹Xianggeng Wei ¹Fei Qin¹

作者信息

1. National Key Laboratory of Solid Rocket Propulsion,Northwestern Polytechnical University,Xi'an,710000,China
2. China Academy of Launch Vehicle Technology,Beijing,100071,China
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摘要

关键词

Oblique detonation engines/Strut injection/Mixing/Combustion/Free jet test

Key words

Oblique detonation engines/Strut injection/Mixing/Combustion/Free jet test

引用本文复制引用

Yiming Zhu,Yunpeng Qin,Dequan Xu,Shaohua Zhu,Jian An,Xianggeng Wei,Fei Qin..Effects and mechanisms of strut injection strategy on mixing and combustion in oblique detonation engines[J].防务技术,2026,58(4):53-68,16.

基金项目

This work was supported by the China Postdoctoral Science Foundation(Grant No.2024M754227),Postdoctoral Fellowship Program(Grade C)of China Postdoctoral Science Foundation(Grant No.GZC20242250),Natural Science Basic Research Program of Shaanxi(Grant No.2025JC-YBQN-690),and Foundation of Na-tional Key Laboratory of Combustion,Flow and Thermo-Structure(Grant No.2025610105000371). （Grant No.2024M754227）

防务技术

ISSN：2214-9147

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