The spatial-temporal evolution of combustion under conditions of low temperature discharge plasma of liquid alcohol injected into an air stream

Stabilization of the combustion of liquid alcohol injected in a drop phase at a mass flow rate of $dm_2/dt=0.5–3$ g/s into a subsonic air jet at a mass flow rate of $dm_1/dt=10–100$ g/s flowing in a submerged space (atmospheric pressure air) was performed under a combined discharge created in a programmable pulse mode.