92 West Dazhi Street
Nan Gang District
Harbin, 150001
China
Harbin Institute of Technology
diffusion and mixing characteristics, Phase transition, liquid kerosene jet, wide-speed-range, supersonic crossflow
thermodynamic analysis, turboexpander engine, chemical non-equilibrium, air-turborocket, supersonic propulsion
fuel temperature, mixing efficiency, Combustion characteristics, swirl combustor