92 West Dazhi Street
Nan Gang District
Harbin, 150001
China
Harbin Institute of Technology
thermodynamic analysis, turboexpander engine, chemical non-equilibrium, air-turborocket, supersonic propulsion
fuel temperature, mixing efficiency, Combustion characteristics, swirl combustor
Penetration characteristics, formula fitting, liquid kerosene transverse jet, evaporation, supersonic combustor