Investigation of flameholding characteristics in a kerosene-fueled scramjet combustor with tandem dual-cavity
Sign Up to like & getrecommendations! 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.… read more here.
Keywords: characteristics kerosene; fueled scramjet; kerosene fueled; flameholding characteristics ... See more keywords
Flameholding characteristics of ethylene-fueled model scramjet in shock tunnel
Sign Up to like & getrecommendations! Published in 2019 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2019.02.022
Abstract: Abstract The flameholding characteristics of a model scramjet were investigated experimentally. Experiments were performed in a shock tunnel at a nominal freestream Mach number of 4. The considered total enthalpy was approximately 1.7 MJ/kg. The test… read more here.
Keywords: injection; inlet; model; cavity ... See more keywords