YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Pre-integrated Nonequilibrium Combustion-Response Mapping for Gas Turbine Emissions

    Source: Journal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 002::page 300
    Author:
    T. Korakianitis
    ,
    R. Dyer
    ,
    N. Subramanian
    DOI: 10.1115/1.1688769
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In gas turbine combustion the gas dynamic and chemical energy release mechanisms have comparable time scales, so that equilibrium chemistry is inadequate for predicting species formation (emissions). In current practice either equilibrium chemical reactions are coupled with experimentally derived empirical equations, or time-consuming computations are used. Coupling nonequilibrium chemistry, fluid dynamic, and initial and boundary condition equations results in large sets of numerically stiff equations; and their time integration demands enormous computational resources. The response modeling approach has been used successfully for large reaction sets. This paper makes two new contributions. First it shows how pre-integration of the heat release maps eliminates the stiffness of the equations. This is a new modification to the response mapping approach, and it performs satisfactorily for non-diffusion systems. Second the theoretical framework is further extended to predict species formation in cases with diffusion, which is applicable to gas turbine combustion systems and others. The methodology to implement this approach to reacting systems, and to gas turbine combustion, is presented. The benefits over other reaction-mapping techniques are discussed.
    keyword(s): Heat , Diffusion (Physics) , Equilibrium (Physics) , Gas turbines , Modeling , Combustion , Equations , Emissions , Fluids , Electromagnetic induction , Temperature , Mechanisms , Density AND Computation ,
    • Download: (131.4Kb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Statistics

      Pre-integrated Nonequilibrium Combustion-Response Mapping for Gas Turbine Emissions

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/130032
    Collections
    • Journal of Engineering for Gas Turbines and Power

    Show full item record

    contributor authorT. Korakianitis
    contributor authorR. Dyer
    contributor authorN. Subramanian
    date accessioned2017-05-09T00:13:01Z
    date available2017-05-09T00:13:01Z
    date copyrightApril, 2004
    date issued2004
    identifier issn1528-8919
    identifier otherJETPEZ-26827#300_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/130032
    description abstractIn gas turbine combustion the gas dynamic and chemical energy release mechanisms have comparable time scales, so that equilibrium chemistry is inadequate for predicting species formation (emissions). In current practice either equilibrium chemical reactions are coupled with experimentally derived empirical equations, or time-consuming computations are used. Coupling nonequilibrium chemistry, fluid dynamic, and initial and boundary condition equations results in large sets of numerically stiff equations; and their time integration demands enormous computational resources. The response modeling approach has been used successfully for large reaction sets. This paper makes two new contributions. First it shows how pre-integration of the heat release maps eliminates the stiffness of the equations. This is a new modification to the response mapping approach, and it performs satisfactorily for non-diffusion systems. Second the theoretical framework is further extended to predict species formation in cases with diffusion, which is applicable to gas turbine combustion systems and others. The methodology to implement this approach to reacting systems, and to gas turbine combustion, is presented. The benefits over other reaction-mapping techniques are discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePre-integrated Nonequilibrium Combustion-Response Mapping for Gas Turbine Emissions
    typeJournal Paper
    journal volume126
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1688769
    journal fristpage300
    journal lastpage305
    identifier eissn0742-4795
    keywordsHeat
    keywordsDiffusion (Physics)
    keywordsEquilibrium (Physics)
    keywordsGas turbines
    keywordsModeling
    keywordsCombustion
    keywordsEquations
    keywordsEmissions
    keywordsFluids
    keywordsElectromagnetic induction
    keywordsTemperature
    keywordsMechanisms
    keywordsDensity AND Computation
    treeJournal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 002
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian