Large Eddy Simulations of Rotating Detonations in Non-Premixed H2-Air Annular Combustor
High fidelity Large Eddy Simulations (LES) are performed on a non-premixed hydrogen-air annular rotating detonation combustor. The simulations utilize a 22-step hydrogen-air reaction mechanism and an existing flow solver that is optimized for high-speed reacting flows. The selected combustor, designed by the US Air Force Research Laboratory (AFRL), has been extensively studied experimentally acros
