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    Inlet Fogging of Gas Turbine Engines—Part II: Fog Droplet Sizing Analysis, Nozzle Types, Measurement, and Testing

    Source: Journal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 003::page 559
    Author:
    Mustapha Chaker
    ,
    Research and Development
    ,
    Cyrus B. Meher-Homji
    ,
    Chief Engineer
    ,
    Thomas Mee
    ,
    Chairman and CEO
    DOI: 10.1115/1.1712982
    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 II of the paper treats the practical aspects of fog nozzle droplet sizing, measurement and testing presenting the information from a gas turbine fogging perspective. This paper describes the different measurement techniques available, covers design aspects of nozzles, provides experimental data on different nozzles, and provides recommendations for a standardized nozzle testing method for gas turbine inlet air fogging.
    keyword(s): Gas turbines , Nozzles AND Sprays ,
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      Inlet Fogging of Gas Turbine Engines—Part II: Fog Droplet Sizing Analysis, Nozzle Types, Measurement, and Testing

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    http://yetl.yabesh.ir/yetl1/handle/yetl/130004
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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#559_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/130004
    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 II of the paper treats the practical aspects of fog nozzle droplet sizing, measurement and testing presenting the information from a gas turbine fogging perspective. This paper describes the different measurement techniques available, covers design aspects of nozzles, provides experimental data on different nozzles, and provides recommendations for a standardized nozzle testing method for gas turbine inlet air fogging.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInlet Fogging of Gas Turbine Engines—Part II: Fog Droplet Sizing Analysis, Nozzle Types, Measurement, and Testing
    typeJournal Paper
    journal volume126
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1712982
    journal fristpage559
    journal lastpage570
    identifier eissn0742-4795
    keywordsGas turbines
    keywordsNozzles AND Sprays
    treeJournal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 003
    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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