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