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    An Annular Pulsed Detonation Combustor Mockup: System Identification and Misfiring Detection

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 004::page 41603
    Author:
    Wolff, Sascha
    ,
    King, Rudibert
    DOI: 10.1115/1.4031320
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An annular pulsed detonation combustor (PDC) basically consists of a number of detonation tubes which are firing in a predetermined sequence into a common downstream annular plenum. Fluctuating initial conditions and fluctuating environmental parameters strongly affect the detonation. Operating such a setup without misfiring is delicate. Misfiring of individual combustion tubes will significantly lower performance or even stop the engine. Hence, an operation of such an engine requires a misfiring detection. Here, a modelbased approach is used which exploits the innovation sequence calculated by a Kalman filter. The model necessary for the Kalman filter is determined based on a modal identification technique. A surrogate, nonreacting experimental setup is considered in order to develop and test these methods.
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      An Annular Pulsed Detonation Combustor Mockup: System Identification and Misfiring Detection

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    http://yetl.yabesh.ir/yetl1/handle/yetl/161014
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorWolff, Sascha
    contributor authorKing, Rudibert
    date accessioned2017-05-09T01:28:08Z
    date available2017-05-09T01:28:08Z
    date issued2016
    identifier issn1528-8919
    identifier othergtp_138_04_041603.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/161014
    description abstractAn annular pulsed detonation combustor (PDC) basically consists of a number of detonation tubes which are firing in a predetermined sequence into a common downstream annular plenum. Fluctuating initial conditions and fluctuating environmental parameters strongly affect the detonation. Operating such a setup without misfiring is delicate. Misfiring of individual combustion tubes will significantly lower performance or even stop the engine. Hence, an operation of such an engine requires a misfiring detection. Here, a modelbased approach is used which exploits the innovation sequence calculated by a Kalman filter. The model necessary for the Kalman filter is determined based on a modal identification technique. A surrogate, nonreacting experimental setup is considered in order to develop and test these methods.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Annular Pulsed Detonation Combustor Mockup: System Identification and Misfiring Detection
    typeJournal Paper
    journal volume138
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4031320
    journal fristpage41603
    journal lastpage41603
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 004
    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