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    A Hyperbolic One-Dimensional Model for Two-Phase Flows in Converging–Diverging Nozzles

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:003::page 179
    Author:
    Cioffi, Andrea
    ,
    Bergamin, Alberto
    ,
    Agromayor, Roberto
    ,
    Haglind, Fredrik
    DOI: 10.1115/1.4069467
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. Partial-evaporation organic Rankine cycle power systems are a promising technology for power generation from low-temperature heat sources such as waste heat and geothermal heat. A specific challenge in two-phase turbines is converging–diverging nozzle design and performance analysis. Existing one-dimensional methods for two-phase flows in nozzles typically rely on space-marching approaches, which are unsuitable for predicting shock waves and thus limit their application to adapted expansion conditions. To address the limitations of existing models, this article presents a new one-dimensional two-phase flow model suitable for capturing shock waves in converging–diverging nozzles. The model employs a finite volume method to solve the balance equations in a conservative form, using time-marching methods to reach the steady-state solution. The predictive performance of the proposed model is validated against experimental data from converging–diverging nozzles using various working fluids, including organic molecules and CO2. The results indicate that the proposed model formulation is suitable for predicting the performance of two-phase nozzles in terms of pressure distribution, critical mass flowrate, and shock wave characteristics across a wide range of operating conditions. These findings suggest that the developed model can be a reliable tool for the preliminary design and analysis of converging–diverging nozzles in two-phase turbines.
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      A Hyperbolic One-Dimensional Model for Two-Phase Flows in Converging–Diverging Nozzles

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4316393
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    contributor authorCioffi, Andrea
    contributor authorBergamin, Alberto
    contributor authorAgromayor, Roberto
    contributor authorHaglind, Fredrik
    date accessioned2026-08-23T08:19:39Z
    date available2026-08-23T08:19:39Z
    date copyright2026/03/01
    date issued2026
    identifier issn0889-504X
    identifier otherturbo-25-1119.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4316393
    description abstractAbstract. Partial-evaporation organic Rankine cycle power systems are a promising technology for power generation from low-temperature heat sources such as waste heat and geothermal heat. A specific challenge in two-phase turbines is converging–diverging nozzle design and performance analysis. Existing one-dimensional methods for two-phase flows in nozzles typically rely on space-marching approaches, which are unsuitable for predicting shock waves and thus limit their application to adapted expansion conditions. To address the limitations of existing models, this article presents a new one-dimensional two-phase flow model suitable for capturing shock waves in converging–diverging nozzles. The model employs a finite volume method to solve the balance equations in a conservative form, using time-marching methods to reach the steady-state solution. The predictive performance of the proposed model is validated against experimental data from converging–diverging nozzles using various working fluids, including organic molecules and CO2. The results indicate that the proposed model formulation is suitable for predicting the performance of two-phase nozzles in terms of pressure distribution, critical mass flowrate, and shock wave characteristics across a wide range of operating conditions. These findings suggest that the developed model can be a reliable tool for the preliminary design and analysis of converging–diverging nozzles in two-phase turbines.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Hyperbolic One-Dimensional Model for Two-Phase Flows in Converging–Diverging Nozzles
    typeJournal Paper
    journal volume148
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4069467
    journal fristpage179
    journal lastpage194
    page16
    treeJournal of Turbomachinery:;2026:;volume( 148 ):;issue:003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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