Numerical Simulation of Non-Equilibrium Two-Phase Wet Steam Flow through an Asymmetric Nozzle

The present study reported of the numerical investigation of a high-speed wet steam flow through an asymmetric nozzle. The spontaneous non-equilibrium homogeneous condensation of wet steam was numerically modeled based on the classical nucleation theory and droplet growth rate equation combined with...

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Main Authors: Miah Md Ashraful Alam, Manabu Takao, Toshiaki Setoguchi
Format: Article
Language:English
Published: MDPI AG 2017-11-01
Series:Fluids
Subjects:
Online Access:https://www.mdpi.com/2311-5521/2/4/63
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spelling doaj-6191ca335a434038abe311a037d189fc2020-11-24T22:33:52ZengMDPI AGFluids2311-55212017-11-01246310.3390/fluids2040063fluids2040063Numerical Simulation of Non-Equilibrium Two-Phase Wet Steam Flow through an Asymmetric NozzleMiah Md Ashraful Alam0Manabu Takao1Toshiaki Setoguchi2Department of Mechanical Engineering, Matsue National College of Technology, Matsue 690-8518, JapanDepartment of Mechanical Engineering, Matsue National College of Technology, Matsue 690-8518, JapanInstitute of Ocean Energy, Saga University, Saga 840-8502, JapanThe present study reported of the numerical investigation of a high-speed wet steam flow through an asymmetric nozzle. The spontaneous non-equilibrium homogeneous condensation of wet steam was numerically modeled based on the classical nucleation theory and droplet growth rate equation combined with the field conservations within the computational fluid dynamics (CFD) code of ANSYS Fluent 13.0. The equations describing droplet formations and interphase change were solved sequentially after solving the main flow conservation equations. The calculations were carried out assuming the flow two-dimensional, compressible, turbulent, and viscous. The SST k-ω model was used for modeling the turbulence within an unstructured mesh solver. The validation of numerical model was accomplished, and the results showed a good agreement between the numerical simulation and experimental data. The effect of spontaneous non-equilibrium condensation on the jet and shock structures was revealed, and the condensation shown a great influence on the jet structure.https://www.mdpi.com/2311-5521/2/4/63compressible flowheat releasenon-equilibrium condensationshock wavesupersonic
collection DOAJ
language English
format Article
sources DOAJ
author Miah Md Ashraful Alam
Manabu Takao
Toshiaki Setoguchi
spellingShingle Miah Md Ashraful Alam
Manabu Takao
Toshiaki Setoguchi
Numerical Simulation of Non-Equilibrium Two-Phase Wet Steam Flow through an Asymmetric Nozzle
Fluids
compressible flow
heat release
non-equilibrium condensation
shock wave
supersonic
author_facet Miah Md Ashraful Alam
Manabu Takao
Toshiaki Setoguchi
author_sort Miah Md Ashraful Alam
title Numerical Simulation of Non-Equilibrium Two-Phase Wet Steam Flow through an Asymmetric Nozzle
title_short Numerical Simulation of Non-Equilibrium Two-Phase Wet Steam Flow through an Asymmetric Nozzle
title_full Numerical Simulation of Non-Equilibrium Two-Phase Wet Steam Flow through an Asymmetric Nozzle
title_fullStr Numerical Simulation of Non-Equilibrium Two-Phase Wet Steam Flow through an Asymmetric Nozzle
title_full_unstemmed Numerical Simulation of Non-Equilibrium Two-Phase Wet Steam Flow through an Asymmetric Nozzle
title_sort numerical simulation of non-equilibrium two-phase wet steam flow through an asymmetric nozzle
publisher MDPI AG
series Fluids
issn 2311-5521
publishDate 2017-11-01
description The present study reported of the numerical investigation of a high-speed wet steam flow through an asymmetric nozzle. The spontaneous non-equilibrium homogeneous condensation of wet steam was numerically modeled based on the classical nucleation theory and droplet growth rate equation combined with the field conservations within the computational fluid dynamics (CFD) code of ANSYS Fluent 13.0. The equations describing droplet formations and interphase change were solved sequentially after solving the main flow conservation equations. The calculations were carried out assuming the flow two-dimensional, compressible, turbulent, and viscous. The SST k-ω model was used for modeling the turbulence within an unstructured mesh solver. The validation of numerical model was accomplished, and the results showed a good agreement between the numerical simulation and experimental data. The effect of spontaneous non-equilibrium condensation on the jet and shock structures was revealed, and the condensation shown a great influence on the jet structure.
topic compressible flow
heat release
non-equilibrium condensation
shock wave
supersonic
url https://www.mdpi.com/2311-5521/2/4/63
work_keys_str_mv AT miahmdashrafulalam numericalsimulationofnonequilibriumtwophasewetsteamflowthroughanasymmetricnozzle
AT manabutakao numericalsimulationofnonequilibriumtwophasewetsteamflowthroughanasymmetricnozzle
AT toshiakisetoguchi numericalsimulationofnonequilibriumtwophasewetsteamflowthroughanasymmetricnozzle
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