Abstract
The results of experimental study of the local characteristics of a butanol near-wall film interacting with a co-current air flow in a supersonic nozzle with a geometric Mach number M = 3.75 are presented. The thickness and velocity of the butanol film front as well as waves on its surface in different cross-sections of the nozzle were measured. The role of the boiling process on the film flow inside the nozzle is studied and its effect on the measured film thickness is shown.
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