Harbin, 150001
China
Harbin Engineering University
digital twin, multi-model fusion, gas turbine, performance adaptation
turbofan engine, starter, start-up, relative humidity, coupled model
rotating detonation, gas turbine, cycle characteristic, component parameters, pressure gain
turbofan engine, start-up, flight environment, component map, low speed zone
digital twin, gas turbine, hybrid modeling, icing condition, performance degradation
Digital twin, icing condition, performance degradation, Gas turbine
