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    Computational Simulation of Gas Turbines: Part 2—Extensible Domain Framework

    Source: Journal of Engineering for Gas Turbines and Power:;2000:;volume( 122 ):;issue: 003::page 377
    Author:
    John A. Reed
    ,
    Abdollah A. Afjeh
    DOI: 10.1115/1.1287489
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the design concepts and object-oriented architecture of Onyx, an extensible domain framework for computational simulation of gas turbine engines. Onyx provides a flexible environment for defining, modifying, and simulating the component-based gas turbine models described in Part 1 of this paper. Using advanced object-oriented technologies such as design patterns and frameworks, Onyx enables users to customize and extend the framework to add new functionality or adapt simulation behavior as required. A customizable visual interface provides high-level symbolic control of propulsion system construction and execution. For computationally-intensive analysis, components may be distributed across heterogeneous computing architectures and operating systems. A distributed gas turbine engine model is developed and simulated to illustrate the use of the framework. [S0742-4795(00)02403-0]
    keyword(s): Engines , Compressors , Manufacturing , Simulation , Design AND Gas turbines ,
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      Computational Simulation of Gas Turbines: Part 2—Extensible Domain Framework

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    http://yetl.yabesh.ir/yetl1/handle/yetl/123654
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    contributor authorJohn A. Reed
    contributor authorAbdollah A. Afjeh
    date accessioned2017-05-09T00:02:21Z
    date available2017-05-09T00:02:21Z
    date copyrightJuly, 2000
    date issued2000
    identifier issn1528-8919
    identifier otherJETPEZ-26797#377_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123654
    description abstractThis paper describes the design concepts and object-oriented architecture of Onyx, an extensible domain framework for computational simulation of gas turbine engines. Onyx provides a flexible environment for defining, modifying, and simulating the component-based gas turbine models described in Part 1 of this paper. Using advanced object-oriented technologies such as design patterns and frameworks, Onyx enables users to customize and extend the framework to add new functionality or adapt simulation behavior as required. A customizable visual interface provides high-level symbolic control of propulsion system construction and execution. For computationally-intensive analysis, components may be distributed across heterogeneous computing architectures and operating systems. A distributed gas turbine engine model is developed and simulated to illustrate the use of the framework. [S0742-4795(00)02403-0]
    publisherThe American Society of Mechanical Engineers (ASME)
    titleComputational Simulation of Gas Turbines: Part 2—Extensible Domain Framework
    typeJournal Paper
    journal volume122
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1287489
    journal fristpage377
    journal lastpage386
    identifier eissn0742-4795
    keywordsEngines
    keywordsCompressors
    keywordsManufacturing
    keywordsSimulation
    keywordsDesign AND Gas turbines
    treeJournal of Engineering for Gas Turbines and Power:;2000:;volume( 122 ):;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
    yabeshDSpacePersian