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    PDA Laser Measurements of Droplet-Laden Flows in a Four-Stage Axial Compressor

    Source: Journal of Turbomachinery:;2022:;volume( 145 ):;issue: 002::page 21013-1
    Author:
    Doerr, Tobias
    ,
    Schuster, Sebastian
    ,
    Brillert, Dieter
    DOI: 10.1115/1.4055767
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Droplet-laden flows play a significant role in the development of turbomachinery. For example, fine water droplets are injected into the flow path of axial compressors to increase the power output of gas turbines by making use of evaporation cooling, often referred to as wet compression. Another example is the ingestion of rain droplets in aircraft engines. Therefore, thermodynamic and aerodynamic measurements of air and liquid are indispensable to better predict the following behavior of the droplets in the gas flow. This article presents a new PDA measurement setup for a droplet-laden four-stage axial compressor to analyze the droplet behavior in swirled flows. To reduce optical disturbances of the laser beam path, liquid films at the casing are suppressed by a boundary layer air injection. Supplementary investigations with this treatment show a negligible influence on the compressor behavior. To minimize refraction effects of the laser beams at the casing window, the laser device with the optical probes can be translated and rotated, thus having 4 degrees-of-freedom. Furthermore, the collected droplet data are compared with a mathematical description of velocity slip in superimposed air flows. For the first time, it can be shown experimentally that droplets smaller than 10 μm attain the velocity of air one stage after injection. For larger droplets, however, deviations from the air Mach number of up to 0.05 remain. In addition, detached liquid films behind the trailing edge of the stator blades with low velocities can be clearly detected.
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      PDA Laser Measurements of Droplet-Laden Flows in a Four-Stage Axial Compressor

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    contributor authorDoerr, Tobias
    contributor authorSchuster, Sebastian
    contributor authorBrillert, Dieter
    date accessioned2023-08-16T18:09:02Z
    date available2023-08-16T18:09:02Z
    date copyright11/3/2022 12:00:00 AM
    date issued2022
    identifier issn0889-504X
    identifier otherturbo_145_2_021013.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4291508
    description abstractDroplet-laden flows play a significant role in the development of turbomachinery. For example, fine water droplets are injected into the flow path of axial compressors to increase the power output of gas turbines by making use of evaporation cooling, often referred to as wet compression. Another example is the ingestion of rain droplets in aircraft engines. Therefore, thermodynamic and aerodynamic measurements of air and liquid are indispensable to better predict the following behavior of the droplets in the gas flow. This article presents a new PDA measurement setup for a droplet-laden four-stage axial compressor to analyze the droplet behavior in swirled flows. To reduce optical disturbances of the laser beam path, liquid films at the casing are suppressed by a boundary layer air injection. Supplementary investigations with this treatment show a negligible influence on the compressor behavior. To minimize refraction effects of the laser beams at the casing window, the laser device with the optical probes can be translated and rotated, thus having 4 degrees-of-freedom. Furthermore, the collected droplet data are compared with a mathematical description of velocity slip in superimposed air flows. For the first time, it can be shown experimentally that droplets smaller than 10 μm attain the velocity of air one stage after injection. For larger droplets, however, deviations from the air Mach number of up to 0.05 remain. In addition, detached liquid films behind the trailing edge of the stator blades with low velocities can be clearly detected.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePDA Laser Measurements of Droplet-Laden Flows in a Four-Stage Axial Compressor
    typeJournal Paper
    journal volume145
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4055767
    journal fristpage21013-1
    journal lastpage21013-11
    page11
    treeJournal of Turbomachinery:;2022:;volume( 145 ):;issue: 002
    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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