Beijing
China
Beijing Power Machinery Institute
Spray combustion, Droplet evaporation, Aero-engine combustor, Lean blow-out, Critical droplet size
Sustainable aviation fuel, Flow reactor, Pyrolysis reaction, Hybrid Chemistry approach (HyChem), NSGA-II
Sustainable aviation fuel, Lean blowout, Swirl spray flame, Atomization performance, Flame dynamic characteristics
Swirl-stabilized gas turbine combustor, Lean blowout, Flame stabilization mechanisms, Turbulent exchange, Precessing vortex core