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    Partial Admission Loss Modeling of Radial Inflow Turbines

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:004
    Author:
    Zhang, Yong
    ,
    Shi, Chenyue
    ,
    Luo, Jin
    ,
    Yang, Chen
    ,
    Yang, Shuhua
    ,
    Yang, Jinguang
    ,
    Li, Yun
    ,
    Sun, Haoqiang
    DOI: 10.1115/1.4070459
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. Radial inflow turbines (RITs) are widely used in aerospace, energy, and chemical industries, and often operate under challenging conditions such as partial admission (PA). However, there is a paucity of fast and accurate empirical models regarding the PA performance prediction of RITs. Therefore, a PA loss model for RIT off-design conditions has been developed in the present study, based on a loss mechanism analysis using numerical simulations. First, the off-design performance of an RIT was simulated using CFD and validated against experimental data. Then, systematic simulations were conducted to analyze the dominant loss mechanisms under PA conditions, namely windage and pumping losses. Inspired by the PA loss modeling approaches used for axial flow turbines (AFTs), a PA loss model for RITs was developed. Correction coefficients were calibrated using CFD data, accounting for key physical parameters including the partial admission ratio, rotational speed, outlet static pressure, and spatial distribution or number of admission segments. The developed model was applied to several RIT cases and validated numerically under varying PA conditions. The results show an average discrepancy of 1.071% in isentropic efficiency between the model predictions and CFD data. The validated PA model exhibits enhanced accuracy and generalizability, providing an effective tool for preliminary design and analysis of RITs at PA conditions.
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      Partial Admission Loss Modeling of Radial Inflow Turbines

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4316622
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    contributor authorZhang, Yong
    contributor authorShi, Chenyue
    contributor authorLuo, Jin
    contributor authorYang, Chen
    contributor authorYang, Shuhua
    contributor authorYang, Jinguang
    contributor authorLi, Yun
    contributor authorSun, Haoqiang
    date accessioned2026-08-23T08:29:19Z
    date available2026-08-23T08:29:19Z
    date copyright2026/04/01
    date issued2026
    identifier issn0889-504X
    identifier otherturbo-25-1076.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4316622
    description abstractAbstract. Radial inflow turbines (RITs) are widely used in aerospace, energy, and chemical industries, and often operate under challenging conditions such as partial admission (PA). However, there is a paucity of fast and accurate empirical models regarding the PA performance prediction of RITs. Therefore, a PA loss model for RIT off-design conditions has been developed in the present study, based on a loss mechanism analysis using numerical simulations. First, the off-design performance of an RIT was simulated using CFD and validated against experimental data. Then, systematic simulations were conducted to analyze the dominant loss mechanisms under PA conditions, namely windage and pumping losses. Inspired by the PA loss modeling approaches used for axial flow turbines (AFTs), a PA loss model for RITs was developed. Correction coefficients were calibrated using CFD data, accounting for key physical parameters including the partial admission ratio, rotational speed, outlet static pressure, and spatial distribution or number of admission segments. The developed model was applied to several RIT cases and validated numerically under varying PA conditions. The results show an average discrepancy of 1.071% in isentropic efficiency between the model predictions and CFD data. The validated PA model exhibits enhanced accuracy and generalizability, providing an effective tool for preliminary design and analysis of RITs at PA conditions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePartial Admission Loss Modeling of Radial Inflow Turbines
    typeJournal Paper
    journal volume148
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4070459
    treeJournal of Turbomachinery:;2026:;volume( 148 ):;issue:004
    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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