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Published in 2017 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2017.08.014
Abstract: Abstract The flameholding characteristics in a kerosene-fueled scramjet combustor with a tandem dual-cavity were investigated experimentally under various inlet stagnation pressure conditions. Flame stabilization locations were judged by the pressure distributions and flame luminescence images.…
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Keywords:
characteristics kerosene;
fueled scramjet;
kerosene fueled;
flameholding characteristics ... See more keywords