Harbin, 150001
China
Harbin Engineering University
digital twin, multi-model fusion, gas turbine, performance adaptation
Large eddy simulation, n-dodecane spray flames, tower-staged combustor, flame root, blow-off, low-temperature chemistry
digital twin, gas turbine, hybrid modeling, icing condition, performance degradation
Gliding arc plasma, swirl flame, Blast furnace gas fuel, Extinction limits, Thermoacoustic characteristics
Digital twin, icing condition, performance degradation, Gas turbine
turbofan engine, start-up, flight environment, component map, low speed zone
Nanosecond pulse, Ignition Delay Time, Blast furnace gas, Plasma-assisted ignition
Sensor fault diagnosis, Data reconciliation, Physics-informed machine learning, Gas turbine