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

    A Modular Code for Real Time Dynamic Simulation of Gas Turbines in Simulink

    Source: Journal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 003::page 506
    Author:
    S. M. Camporeale
    ,
    B. Fortunato
    ,
    M. Mastrovito
    DOI: 10.1115/1.2132383
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A high-fidelity real-time simulation code based on a lumped, nonlinear representation of gas turbine components is presented. The code is a general-purpose simulation software environment useful for setting up and testing control equipments. The mathematical model and the numerical procedure are specially developed in order to efficiently solve the set of algebraic and ordinary differential equations that describe the dynamic behavior of gas turbine engines. For high-fidelity purposes, the mathematical model takes into account the actual composition of the working gases and the variation of the specific heats with the temperature, including a stage-by-stage model of the air-cooled expansion. The paper presents the model and the adopted solver procedure. The code, developed in Matlab-Simulink using an object-oriented approach, is flexible and can be easily adapted to any kind of plant configuration. Simulation tests of the transients after load rejection have been carried out for a single-shaft heavy-duty gas turbine and a double-shaft aero-derivative industrial engine. Time plots of the main variables that describe the gas turbine dynamic behavior are shown and the results regarding the computational time per time step are discussed.
    keyword(s): Temperature , Simulation , Gas turbines , Turbines , Compressors , Flow (Dynamics) AND Pressure ,
    • Download: (534.9Kb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Statistics

      A Modular Code for Real Time Dynamic Simulation of Gas Turbines in Simulink

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/133652
    Collections
    • Journal of Engineering for Gas Turbines and Power

    Show full item record

    contributor authorS. M. Camporeale
    contributor authorB. Fortunato
    contributor authorM. Mastrovito
    date accessioned2017-05-09T00:19:47Z
    date available2017-05-09T00:19:47Z
    date copyrightJuly, 2006
    date issued2006
    identifier issn1528-8919
    identifier otherJETPEZ-26914#506_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133652
    description abstractA high-fidelity real-time simulation code based on a lumped, nonlinear representation of gas turbine components is presented. The code is a general-purpose simulation software environment useful for setting up and testing control equipments. The mathematical model and the numerical procedure are specially developed in order to efficiently solve the set of algebraic and ordinary differential equations that describe the dynamic behavior of gas turbine engines. For high-fidelity purposes, the mathematical model takes into account the actual composition of the working gases and the variation of the specific heats with the temperature, including a stage-by-stage model of the air-cooled expansion. The paper presents the model and the adopted solver procedure. The code, developed in Matlab-Simulink using an object-oriented approach, is flexible and can be easily adapted to any kind of plant configuration. Simulation tests of the transients after load rejection have been carried out for a single-shaft heavy-duty gas turbine and a double-shaft aero-derivative industrial engine. Time plots of the main variables that describe the gas turbine dynamic behavior are shown and the results regarding the computational time per time step are discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Modular Code for Real Time Dynamic Simulation of Gas Turbines in Simulink
    typeJournal Paper
    journal volume128
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2132383
    journal fristpage506
    journal lastpage517
    identifier eissn0742-4795
    keywordsTemperature
    keywordsSimulation
    keywordsGas turbines
    keywordsTurbines
    keywordsCompressors
    keywordsFlow (Dynamics) AND Pressure
    treeJournal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 003
    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