Author:
Li Xipeng,Liu Weidong,Pan Yu,Yang Leichao,An Bin,Zhu Jiajian
Funder
National Natural Science Foundation of China
Reference23 articles.
1. Experimental Investigation of Mixing and Ignition of Transverse Jets in Supersonic Crossflows (Ph.D. thesis);Ben-Yakar,2000
2. J.L. Le, S.H. Yang, X.Y. Wang, H.B. Li, Analysis and correlation of flame stability limits in supersonic flow with cavity flameholder, in: Proceedings of the 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, AIAA-2012-5948, Tours, France, 2012
3. Effect of cavity con figuration on kerosene spark ignition in a scramjet combustor at Ma 4.5 flight condition;Bao;Acta Astronaut.,2015
4. Experimental investigation on ignition schemes of a supersonic combustor with the rearwall-expansion cavity;Cai;Acta Astronaut.,2016
5. Large eddy simulation of the fuel transport and mixing process in a scramjet combustor with rearwall-expansion cavity;Cai;Acta Astronaut.,2016
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