Shockwave effects on supersonic combustion using hypermixer struts
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DOI: 10.1063/1.5128677
Abstract: This study describes combustion features due to streamwise vorticity when using hypermixer struts at Mach numbers of 2.5 and 3.5. Two types of struts are used with hydrogen fuel (at an equivalence ratio of 0.4)… read more here.
Keywords: supersonic combustion; strut; combustion; using hypermixer ... See more keywords
Modeling of Supersonic Combustion Systems for Sustained Hypersonic Flight
Sign Up to like & getrecommendations! Published in 2017 at "Energies"
DOI: 10.3390/en10111900
Abstract: Through Computational Fluid Dynamics and validation, an optimal scramjet combustor has been designed based on twin-strut Hydrogen injection to sustain flight at a desired speed of Mach 8. An investigation undertaken into the efficacy of… read more here.
Keywords: supersonic combustion; systems sustained; combustion; modeling supersonic ... See more keywords