Combustion modes of hydrogen jet combustion in a cavity-based supersonic combustor
By Hong-bo Wang, Zhenguo Wang, Mingbo Sun, Haiyan Wu. 2013
308 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/744dc236ca46cb1c0359eb1f975f53387f80cd95
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In Aerospace Engineering
In Computational Mechanics
Citations in the corpus
- Large eddy simulation of a hydrogen-fueled scramjet combustor with dual cavity (2015, methodology): “When used as an integrated fuel injection/flameholding approach [2], cavity flameholders have become even more attractive in supersonic combustors and received more and more attention [3–14].”
- Review of cavity-stabilized combustion for scramjet applications (2014, background): “Wang et al.23 observed large spreading angle of the reaction zone up to 30 degree in the experiment.”