Study of the gas-droplet outflow from a microchannel nozzle device

High-speed shadow imaging of a gas-droplet flow from a microchannel nozzle device was performed by varying the liquid flow rate from 1 to 50 ml/min and the gas pressure drop from 0.5 to 8 bar. For this purpose, an optical system with a stereomicroscope was assembled to ensure a large depth of field and relatively high resolution. The outflow was studied for two types of nozzles: a three-nozzle device with an internal channel diameter of 200 µm and a custom-made nozzle with a microchannel silicon membrane of 243 µm thickness and a microchannel size of 10×10 µm. Spray angles for a single nozzle and an angle averaged over three nozzles were determined. Dependences of the angles on liquid flow rate for each pressure drop and dependences on pressure drop with varying liquid flow rate were obtained. It is shown that a uniform gas-droplet flow can be organized at the nozzle edge with small droplets using a microchannel membrane.

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Publication Details

Journal
Thermophysics and Aeromechanics
Published
2025-03-11
DOI
https://doi.org/10.1134/s0869864324040115
Primary Topic
Combustion and flame dynamics
Type
article
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article

Study of the gas-droplet outflow from a microchannel nozzle device

Elizaveta Ya. Gatapova
Thermophysics and Aeromechanics
Combustion and flame dynamics
article

Study of the gas-droplet outflow from a microchannel nozzle device

Elizaveta Ya. Gatapova
article en

Abstract

High-speed shadow imaging of a gas-droplet flow from a microchannel nozzle device was performed by varying the liquid flow rate from 1 to 50 ml/min and the gas pressure drop from 0.5 to 8 bar. For this purpose, an optical system with a stereomicroscope was assembled to ensure a large depth of field and relatively high resolution. The outflow was studied for two types of nozzles: a three-nozzle device with an internal channel diameter of 200 µm and a custom-made nozzle with a microchannel silicon membrane of 243 µm thickness and a microchannel size of 10×10 µm. Spray angles for a single nozzle and an angle averaged over three nozzles were determined. Dependences of the angles on liquid flow rate for each pressure drop and dependences on pressure drop with varying liquid flow rate were obtained. It is shown that a uniform gas-droplet flow can be organized at the nozzle edge with small droplets using a microchannel membrane.

Thermophysics and AeromechanicsVol. 31(4)
Novosibirsk State University (RU), Institute of Thermophysics (RU)
Affordable and clean energy
Openalex Percentile: Top 95%
Combustion and flame dynamics
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Study of the gas-droplet outflow from a microchannel nozzle device — Elizaveta Ya. Gatapova · Thermophysics and Aeromechanics (2025) | TGRS Research Map | TGRS