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    Influence of Geometric Variations of an Inlet Cover Bleed System on Inducer Performance for an Axial Pump Operating Under Cavitating Conditions

    Source: Journal of Fluids Engineering:;2022:;volume( 144 ):;issue: 008::page 81402-1
    Author:
    Lundgreen, Ryan K.
    ,
    Maynes, Daniel
    ,
    Gorrell, Steve
    ,
    Oliphant, Kerry
    DOI: 10.1115/1.4053648
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A stability control device (SCD) is a passive inlet cover treatment that can be applied to high suction performance inducers. Significant improvements in stability have been observed when an inducer operates with an SCD, including suppression of backflow at the leading edge of the inducer at low off-design flow coefficients. This is possible because of a local increase in mass flow at the leading edge of the pump, which allows an inducer to operate with an incidence near the design point value over a wide range of flow coefficients. In this paper, the suction performance of several inducers was explored with several different SCD geometries and at different flow coefficients. Specifically, five different SCD geometries were considered to explore the influence that SCD bleed slot width and resistance to flow through the SCD channel have on inducer performance. Further, removal of tangential velocity of the energized fluid transporting through the SCD channel was considered for some scenarios to highlight the impact of swirl on inducer performance. The results reveal that for all inducers and SCD combinations considered, the most important factor affecting the mass flow through the SCD, and subsequent mass flow gain, is the inlet diffusion of the inducer. This holds for both single-phase and multiphase scenarios. Further, the cavitation number where cavitation first starts to develop in the blade throat passage of the inducer is primarily dependent on the inlet blade angle and not the SCD geometry. Consequently, the shape of the cavitation breakdown curve is largely determined by the inducer blade angle.
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      Influence of Geometric Variations of an Inlet Cover Bleed System on Inducer Performance for an Axial Pump Operating Under Cavitating Conditions

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4284876
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    contributor authorLundgreen, Ryan K.
    contributor authorMaynes, Daniel
    contributor authorGorrell, Steve
    contributor authorOliphant, Kerry
    date accessioned2022-05-08T09:13:36Z
    date available2022-05-08T09:13:36Z
    date copyright3/7/2022 12:00:00 AM
    date issued2022
    identifier issn0098-2202
    identifier otherfe_144_08_081402.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4284876
    description abstractA stability control device (SCD) is a passive inlet cover treatment that can be applied to high suction performance inducers. Significant improvements in stability have been observed when an inducer operates with an SCD, including suppression of backflow at the leading edge of the inducer at low off-design flow coefficients. This is possible because of a local increase in mass flow at the leading edge of the pump, which allows an inducer to operate with an incidence near the design point value over a wide range of flow coefficients. In this paper, the suction performance of several inducers was explored with several different SCD geometries and at different flow coefficients. Specifically, five different SCD geometries were considered to explore the influence that SCD bleed slot width and resistance to flow through the SCD channel have on inducer performance. Further, removal of tangential velocity of the energized fluid transporting through the SCD channel was considered for some scenarios to highlight the impact of swirl on inducer performance. The results reveal that for all inducers and SCD combinations considered, the most important factor affecting the mass flow through the SCD, and subsequent mass flow gain, is the inlet diffusion of the inducer. This holds for both single-phase and multiphase scenarios. Further, the cavitation number where cavitation first starts to develop in the blade throat passage of the inducer is primarily dependent on the inlet blade angle and not the SCD geometry. Consequently, the shape of the cavitation breakdown curve is largely determined by the inducer blade angle.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInfluence of Geometric Variations of an Inlet Cover Bleed System on Inducer Performance for an Axial Pump Operating Under Cavitating Conditions
    typeJournal Paper
    journal volume144
    journal issue8
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.4053648
    journal fristpage81402-1
    journal lastpage81402-9
    page9
    treeJournal of Fluids Engineering:;2022:;volume( 144 ):;issue: 008
    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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