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Mach number effect on droplet phase angular distribution behind a nozzle under near-wall liquid film outflow with co-current gas flow into vacuum
Author(s) -
Yu.N. Vyazov,
V. G. Prikhodko,
I. V. Yarygin
Publication year - 2021
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1867/1/012003
Subject(s) - nozzle , mach number , outflow , mechanics , current (fluid) , materials science , choked flow , flow (mathematics) , flow visualization , supersonic speed , jet (fluid) , two phase flow , optics , phase (matter) , chemistry , physics , thermodynamics , meteorology , organic chemistry
The paper is devoted to experimental study of near-wall ethanol film outflow with high-velocity co-current air flow from sonic and supersonic nozzles into vacuum. Using the developed measurement techniques (droplet phase flow structure visualization, deposition of droplets on paper substrates, spectrophotometry method), the effect of the nozzle Mach number on angular distribution of droplet phase in the central and the peripheral flow regions behind the nozzle exit is established.

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