The shock-assisted self-ignition behavior and combustion transition mechanisms in a Mach 8 scramjet combustor
2025 · Combustion and Flame · 8 citations
https://doi.org/10.1016/j.combustflame.2025.114721
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Chenxiang Zhao is an academic researcher from National University of Defense Technology. The author has contributed to research in topics: Computational Fluid Dynamics and Aerodynamics & Combustion and flame dynamics & Rocket and propulsion systems research. The author has an h-index of 3, co-authored 8 publications.
ORCID: 0009-0003-6387-1196https://doi.org/10.1016/j.combustflame.2025.114721
https://doi.org/10.2514/1.j065087
https://doi.org/10.1016/j.applthermaleng.2025.128318
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