Litcius/Paper detail

Effects of inlet air temperature and mass flow rate on the performance of a liquid kerosene/air rotating detonation ramjet combustor

Xiafei Li, Jin Wu, Jianzhong Li, Qian Yao, Qiongyao Qin, Yuan Li

2025Acta Astronautica5 citationsDOI

Topics & Concepts

DetonationRamjetCombustorCombustionDeflagration to detonation transitionMechanicsMaterials scienceInletMass flowMass flow rateVolumetric flow rateMach numberTotal air temperatureThrustDecoupling (probability)ThermodynamicsCombustion chamberNuclear engineeringFlow (mathematics)Aerospace engineeringStagnation temperatureCombustion and Detonation ProcessesEnergetic Materials and CombustionRocket and propulsion systems research