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    Inlet Fogging of Gas Turbine Engines—Part I: Fog Droplet Thermodynamics, Heat Transfer, and Practical Considerations

    Source: Journal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 003::page 545
    Author:
    Mustapha Chaker
    ,
    Research and Development
    ,
    Cyrus B. Meher-Homji
    ,
    Chief Engineer
    ,
    Thomas Mee
    ,
    Chairman and CEO
    DOI: 10.1115/1.1712981
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The inlet fogging of gas turbine engines for power augmentation has seen increasing application over the past decade yet not a single technical paper treating the physics and engineering of the fogging process, droplet size measurement, droplet kinetics, or the duct behavior of droplets, from a gas turbine perspective, is available. This paper provides the results of extensive experimental and theoretical studies conducted over several years coupled with practical aspects learned in the implementation of nearly 500 inlet fogging systems on gas turbines ranging in power from 5 to 250 MW. Part I of the paper covers the underlying theory of droplet thermodynamics and heat transfer, and provides several practical pointers relating to the implementation and application of inlet fogging to gas turbine engines.
    keyword(s): Temperature , Gas turbines , Nozzles , Ducts , Water , Heat transfer , Compressors , Thermodynamics , Heat AND Evaporation ,
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      Inlet Fogging of Gas Turbine Engines—Part I: Fog Droplet Thermodynamics, Heat Transfer, and Practical Considerations

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    http://yetl.yabesh.ir/yetl1/handle/yetl/130003
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorMustapha Chaker
    contributor authorResearch and Development
    contributor authorCyrus B. Meher-Homji
    contributor authorChief Engineer
    contributor authorThomas Mee
    contributor authorChairman and CEO
    date accessioned2017-05-09T00:12:58Z
    date available2017-05-09T00:12:58Z
    date copyrightJuly, 2004
    date issued2004
    identifier issn1528-8919
    identifier otherJETPEZ-26829#545_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/130003
    description abstractThe inlet fogging of gas turbine engines for power augmentation has seen increasing application over the past decade yet not a single technical paper treating the physics and engineering of the fogging process, droplet size measurement, droplet kinetics, or the duct behavior of droplets, from a gas turbine perspective, is available. This paper provides the results of extensive experimental and theoretical studies conducted over several years coupled with practical aspects learned in the implementation of nearly 500 inlet fogging systems on gas turbines ranging in power from 5 to 250 MW. Part I of the paper covers the underlying theory of droplet thermodynamics and heat transfer, and provides several practical pointers relating to the implementation and application of inlet fogging to gas turbine engines.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInlet Fogging of Gas Turbine Engines—Part I: Fog Droplet Thermodynamics, Heat Transfer, and Practical Considerations
    typeJournal Paper
    journal volume126
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1712981
    journal fristpage545
    journal lastpage558
    identifier eissn0742-4795
    keywordsTemperature
    keywordsGas turbines
    keywordsNozzles
    keywordsDucts
    keywordsWater
    keywordsHeat transfer
    keywordsCompressors
    keywordsThermodynamics
    keywordsHeat AND Evaporation
    treeJournal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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