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    The Use of a Hybrid Computer in the Optimization of Gas Turbine Control Parameters

    Source: Journal of Engineering for Gas Turbines and Power:;1973:;volume( 095 ):;issue: 003::page 257
    Author:
    H. I. H. Saravanamuttoo
    ,
    B. D. MacIsaac
    DOI: 10.1115/1.3445731
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper discusses the hybrid computer simulation of a single-spool turbojet engine. The problem is approached from the viewpoint of engineering thermodynamics, using the normal compressor and turbine characteristics. This was found to yield an extremely flexible simulation capable of operation over the entire running range. The simulation was used to investigate methods of improving the thrust response and it was found that a detailed insight into the engine dynamics permitted a significant improvement in thrust response.
    keyword(s): Dynamics (Mechanics) , Thermodynamics , Computer simulation , Engines , Compressors , Thrust , Simulation , Gas turbines , Optimization , Turbines , Computers AND Turbojets ,
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      The Use of a Hybrid Computer in the Optimization of Gas Turbine Control Parameters

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/163773
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorH. I. H. Saravanamuttoo
    contributor authorB. D. MacIsaac
    date accessioned2017-05-09T01:36:22Z
    date available2017-05-09T01:36:22Z
    date copyrightJuly, 1973
    date issued1973
    identifier issn1528-8919
    identifier otherJETPEZ-26704#257_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/163773
    description abstractThis paper discusses the hybrid computer simulation of a single-spool turbojet engine. The problem is approached from the viewpoint of engineering thermodynamics, using the normal compressor and turbine characteristics. This was found to yield an extremely flexible simulation capable of operation over the entire running range. The simulation was used to investigate methods of improving the thrust response and it was found that a detailed insight into the engine dynamics permitted a significant improvement in thrust response.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Use of a Hybrid Computer in the Optimization of Gas Turbine Control Parameters
    typeJournal Paper
    journal volume95
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3445731
    journal fristpage257
    journal lastpage264
    identifier eissn0742-4795
    keywordsDynamics (Mechanics)
    keywordsThermodynamics
    keywordsComputer simulation
    keywordsEngines
    keywordsCompressors
    keywordsThrust
    keywordsSimulation
    keywordsGas turbines
    keywordsOptimization
    keywordsTurbines
    keywordsComputers AND Turbojets
    treeJournal of Engineering for Gas Turbines and Power:;1973:;volume( 095 ):;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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