2D and 3D numerical modelling of internal flow of Pressure-swirl atomizer
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F18%3APU130212" target="_blank" >RIV/00216305:26210/18:PU130212 - isvavai.cz</a>
Result on the web
<a href="https://www.epj-conferences.org/articles/epjconf/abs/2019/18/epjconf_efm18_02055/epjconf_efm18_02055.html" target="_blank" >https://www.epj-conferences.org/articles/epjconf/abs/2019/18/epjconf_efm18_02055/epjconf_efm18_02055.html</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1051/epjconf/201921302055" target="_blank" >10.1051/epjconf/201921302055</a>
Alternative languages
Result language
angličtina
Original language name
2D and 3D numerical modelling of internal flow of Pressure-swirl atomizer
Original language description
This paper compares 2D axisymmetric and 3D numerical models used to predict the internal flow of a pressure-swirl atomizer using a commercial software Ansys Fluent 18.1. The computed results are compared with experimental data in terms of spray cone angle (SCA), discharge coefficient (CD), internal air-core dimensions and swirl velocity profile. The swirl velocity was experimentally studied using a Laser Doppler Anemometry in a scaled transparent model of the atomizer. The internal air-core was visualized at high temporal and spatial resolution by a high-speed camera with backlit illumination. The internal flow was numerically treated as transient two-phase flow. The gas-liquid interface was captured with Volume of Fluid scheme. The numerical solver used both laminar and turbulent approach. Turbulence was modelled using k-ε, k-ω, Reynolds Stress model (RSM) and coarse Large Eddy Simulation (LES). The laminar solver was capable to predict all the parameters with an error less than 5% compared with the experimental results in both 2D and 3D simulation. However, it overpredicted the velocity of the discharged liquid sheet. The LES model performed similarly to the laminar solver, but the liquid sheet velocity was 10% lower. The two-equation models k-ε and k-ω overpredicted the turbulence viscosity and the internal air-core was not predicted
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
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OECD FORD branch
20302 - Applied mechanics
Result continuities
Project
Result was created during the realization of more than one project. More information in the Projects tab.
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2019
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
EFM18 – Experimental Fluid Mechanics 2018
ISBN
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ISSN
2100-014X
e-ISSN
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Number of pages
6
Pages from-to
1-6
Publisher name
EDP Sciences
Place of publication
neuveden
Event location
Praha
Event date
Nov 13, 2018
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
000504642200056