Interaction of a liquid jet with a co-current gas flow inside the nozzle and under ejection into vacuum

Abstract The structure of a gas-droplet flow arising under gas outflow with liquid jet injected into it from supersonic nozzle vacuum is studied experimentally. Possibility the control in order to obtain droplets certain size, composition, and velocity, considered. was co-current prechamber then flowed out chamber form jet. Using developed technique droplet deposition on paper substrates, effect Reynolds number pressure angular distribution phase behind exit investigated.