Modeling of Supersonic Combustion Systems for Sustained Hypersonic Flight
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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