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    Dynamic Similarity in Turbine Deposition Testing and the Role of Pressure

    Source: Journal of Engineering for Gas Turbines and Power:;2018:;volume( 140 ):;issue: 010::page 102605
    Author:
    Sacco, C.
    ,
    Bowen, C.
    ,
    Lundgreen, R.
    ,
    Bons, J. P.
    ,
    Ruggiero, E.
    ,
    Allen, J.
    ,
    Bailey, J.
    DOI: 10.1115/1.4038550
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The role of absolute pressure in deposition testing is reviewed from first principles. Relevant dimensionless parameters for deposition testing are developed and dynamic similarity conditions are assessed in detail. Criteria for establishing appropriate conditions for laboratory studies of deposition are established pursuant to the similarity variables. The role of pressure is particularly singled out for consideration relative to other variables such as temperature, particle size, and test article geometry/scaling. A case study is presented for deposition in a generic array of impinging jets. A fixed quantity (2 g) of 0–10 μ Arizona road dust (ARD) is delivered to the impingement array at three different temperatures (290, 500, and 725 K) and at fixed pressure ratio. Deposition results are presented for operating pressures from 1 to 15 atm. Surface scans show that the height of deposit cones at the impingement sites decreases with increasing pressure at constant temperature and pressure ratio. This reduction is explained by the lower “effective” Stokes number that occurs at high particle Reynolds numbers, yielding fewer particle impacts at high pressure. A companion computational fluid dynamics (CFD) study identifies the additional role of Reynolds number in both the impingement hole losses and the shear layer thickness.
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      Dynamic Similarity in Turbine Deposition Testing and the Role of Pressure

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4251292
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorSacco, C.
    contributor authorBowen, C.
    contributor authorLundgreen, R.
    contributor authorBons, J. P.
    contributor authorRuggiero, E.
    contributor authorAllen, J.
    contributor authorBailey, J.
    date accessioned2019-02-28T10:58:17Z
    date available2019-02-28T10:58:17Z
    date copyright7/5/2018 12:00:00 AM
    date issued2018
    identifier issn0742-4795
    identifier othergtp_140_10_102605.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4251292
    description abstractThe role of absolute pressure in deposition testing is reviewed from first principles. Relevant dimensionless parameters for deposition testing are developed and dynamic similarity conditions are assessed in detail. Criteria for establishing appropriate conditions for laboratory studies of deposition are established pursuant to the similarity variables. The role of pressure is particularly singled out for consideration relative to other variables such as temperature, particle size, and test article geometry/scaling. A case study is presented for deposition in a generic array of impinging jets. A fixed quantity (2 g) of 0–10 μ Arizona road dust (ARD) is delivered to the impingement array at three different temperatures (290, 500, and 725 K) and at fixed pressure ratio. Deposition results are presented for operating pressures from 1 to 15 atm. Surface scans show that the height of deposit cones at the impingement sites decreases with increasing pressure at constant temperature and pressure ratio. This reduction is explained by the lower “effective” Stokes number that occurs at high particle Reynolds numbers, yielding fewer particle impacts at high pressure. A companion computational fluid dynamics (CFD) study identifies the additional role of Reynolds number in both the impingement hole losses and the shear layer thickness.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDynamic Similarity in Turbine Deposition Testing and the Role of Pressure
    typeJournal Paper
    journal volume140
    journal issue10
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4038550
    journal fristpage102605
    journal lastpage102605-12
    treeJournal of Engineering for Gas Turbines and Power:;2018:;volume( 140 ):;issue: 010
    contenttypeFulltext
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