Theoretical Analyses of Drop Size in Impinging and Effervescent Liquid Jets

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F23%3APU150036" target="_blank" >RIV/00216305:26210/23:PU150036 - isvavai.cz</a>
Result on the web
<a href="https://arc.aiaa.org/doi/10.2514/6.2023-4247" target="_blank" >https://arc.aiaa.org/doi/10.2514/6.2023-4247</a>
DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Theoretical Analyses of Drop Size in Impinging and Effervescent Liquid Jets
Original language description
Impinging and effervescent injections are used to generate small droplets in fuel and other sprays. For example, multiple streams of fuel and oxidizers are injected at collision angles in rocket combustion chambers. Effervescent atomizers send both the liquid and air streams within the injector, and thus can be considered as an internal analog of liquid jets in co-flow of air. The interaction of the air and liquid enhances the final drop size for a similar reason. The drop size during atomization processes in various injection geometries has been considered by Lee and co-workers [1-5]. In this work, we apply the same theoretical basis to impinging and effervescent liquid jets.
Czech name
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Czech description
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Project
<a href="/en/project/GA22-17806S" target="_blank" >GA22-17806S: Advanced liquid film and spray systems for gas cleaning and sorption purposes</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2023
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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