Assessment of Cavitation Models for Compressible Flows Inside a Nozzle
Kumar, A., Ghobadian, A. & Nouri, J. M. ORCID: 0000-0001-8610-3737 (2020). Assessment of Cavitation Models for Compressible Flows Inside a Nozzle. Fluids, 5(3), article number 134. doi: 10.3390/fluids5030134
Abstract
This study assessed two cavitation models for compressible cavitating flows within a single hole nozzle. The models evaluated were SS (Schnerr and Sauer) and ZGB (Zwart-Gerber-Belamri) using realizable k-epsilon turbulent model, which was found to be the most appropriate model to use for this flow. The liquid compressibility was modeled using the Tait equation, and the vapor compressibility was modeled using the ideal gas law. Compressible flow simulation results showed that the SS model failed to capture the flow physics with a weak agreement with experimental data, while the ZGB model predicted the flow much better. Modeling vapor compressibility improved the distribution of the cavitating vapor across the nozzle with an increase in vapor volume compared to that of the incompressible assumption, particularly in the core region which resulted in a much better quantitative and qualitative agreement with the experimental data. The results also showed the prediction of a normal shockwave downstream of the cavitation region where the local flow transforms from supersonic to subsonic because of an increase in the local pressure.
Publication Type: | Article |
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Additional Information: | This is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. |
Publisher Keywords: | cavitation; single nozzle; compressible flow; CFD; cavitation model; predictions; model validation; shockwave |
Subjects: | T Technology > TJ Mechanical engineering and machinery T Technology > TL Motor vehicles. Aeronautics. Astronautics |
Departments: | School of Science & Technology > Engineering |
SWORD Depositor: |
Available under License Creative Commons: Attribution International Public License 4.0.
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