Beijing, 100084
China
Tsinghua University
Spray combustion, Droplet evaporation, Aero-engine combustor, Lean blow-out, Critical droplet size
deposition prediction, kinetic model, oxidative deposition, aviation fuel, fuel cooling
Sustainable aviation fuel, Flow reactor, Pyrolysis reaction, Hybrid Chemistry approach (HyChem), NSGA-II
Carbon deposition, Venturi, Swirl combustion, Coking, Aviation kerosene
Swirl-stabilized gas turbine combustor, Lean blowout, Flame stabilization mechanisms, Turbulent exchange, Precessing vortex core