2D Euler modeling of rotating detonation combustion in preparation for turbomachinery matching
View Video Presentation: https://doi. org/10.2514/6.2022-0836. vid A two dimensional, time
resolved reactive Euler solver is applied to simulate the flow field of a rotating detonation
combustor (RDC). Simulations are performed for two different air injection area ratios of
(14.4%, 28.7%) in combination with two different fuel injection area ratios (1%, 1.5%) and
five different outlet throat to annulus area ratios (100%, 84%, 75%, 67%, 50%) over a mass
flux range of 60 kg/s/m² to 290 kg/s/m². Air and fuel injection are modeled independently …
resolved reactive Euler solver is applied to simulate the flow field of a rotating detonation
combustor (RDC). Simulations are performed for two different air injection area ratios of
(14.4%, 28.7%) in combination with two different fuel injection area ratios (1%, 1.5%) and
five different outlet throat to annulus area ratios (100%, 84%, 75%, 67%, 50%) over a mass
flux range of 60 kg/s/m² to 290 kg/s/m². Air and fuel injection are modeled independently …