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Laser ablation ignition modes in a cavity-based supersonic combustor

Jianheng JI Zun CAI Taiyu WANG Yifu TIAN Mingbo SUN Jiajian ZHU Zhenguo WANG

中国航空学报(英文版)2025,Vol.38Issue(4):112-126,15.
中国航空学报(英文版)2025,Vol.38Issue(4):112-126,15.DOI:10.1016/j.cja.2024.11.003

Laser ablation ignition modes in a cavity-based supersonic combustor

Laser ablation ignition modes in a cavity-based supersonic combustor

Jianheng JI 1Zun CAI 1Taiyu WANG 1Yifu TIAN 1Mingbo SUN 1Jiajian ZHU 1Zhenguo WANG1

作者信息

  • 1. Hypersonic Technology Laboratory,National University of Defense Technology,Changsha 410073,China
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摘要

关键词

Laser ablation/Ignition mode/Supersonic combustor/Flame propagation/Cavity

Key words

Laser ablation/Ignition mode/Supersonic combustor/Flame propagation/Cavity

引用本文复制引用

Jianheng JI,Zun CAI,Taiyu WANG,Yifu TIAN,Mingbo SUN,Jiajian ZHU,Zhenguo WANG..Laser ablation ignition modes in a cavity-based supersonic combustor[J].中国航空学报(英文版),2025,38(4):112-126,15.

基金项目

This study was supported by the National Natural Science Foundation of China(Nos.12272408 and 11925207)and the Natural Science Foundation for Distinguished Young Schol-ars of Hunan Province,China(No.2024J12057). (Nos.12272408 and 11925207)

中国航空学报(英文版)

1000-9361

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