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
Cone-strut flameholder, Injection strategies, Minimum equivalence ratio for ignition, Ignition delay time, Ignition pathway
diffusion and mixing characteristics, liquid-kerosene, shock wave, Evaporation, supersonic combustor
thermodynamic analysis, turboexpander engine, chemical non-equilibrium, air-turborocket, supersonic propulsion
Supersonic combustion, multi-strut, liquid kerosene, shock wave, flow combustion coupling, flame diffusion characteristics
Penetration characteristics, formula fitting, liquid kerosene transverse jet, evaporation, supersonic combustor
Strut/wall combined-staged injection, Combustion performance optimization, Axisymmetric variable geometry combustor, Low Mach number, Wall injection position effects
Supersonic combustor, Bluff body flame holder, Ignitor position, Time series analysis, Plasma ignitor
diffusion and mixing characteristics, injection momentum, evaporation, shock wave, supersonic combustor
Linear variation of kerosene, pressure distribution characteristics, intense heat release zone movement, critical kerosene equivalence ratios
Ignitor position, Flame establishment mode, Time series analysis, Plasma ignitor, Supersonic shear layer
Ammonia, Hydrogen, Swirling flames, CRN, Chemical kinetic