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    A Fiber Optic Probe for Gas Total Temperature Measurement in Turbomachinery

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 004::page 635
    Author:
    S. R. Kidd
    ,
    M. A. Cherrett
    ,
    K. S. Chana
    ,
    J. S. Barton
    ,
    P. Meredith
    ,
    J. D. C. Jones
    DOI: 10.1115/1.2836582
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the design, operation, construction, and demonstration of a new type of high-bandwidth unsteady temperature sensor based on fiber optics, and capable of operating in a high-speed multistage research compressor with flow representative of jet engine conditions. The sensing element is an optical coating of zinc selenide deposited on the end of an optical fiber. During evaluation in aerodynamic testing, a 1 K gas temperature resolution was demonstrated at 9.6 kHz and an upper bandwidth limit of 36 kHz achieved.
    keyword(s): Flow (Dynamics) , Temperature , Fibers , Temperature measurement , Compressors , Construction , Optical coatings , Resolution (Optics) , Design , Testing , Jet engines , Optical fiber , Probes , Temperature sensors AND Turbomachinery ,
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      A Fiber Optic Probe for Gas Total Temperature Measurement in Turbomachinery

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/116120
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    • Journal of Turbomachinery

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    contributor authorS. R. Kidd
    contributor authorM. A. Cherrett
    contributor authorK. S. Chana
    contributor authorJ. S. Barton
    contributor authorP. Meredith
    contributor authorJ. D. C. Jones
    date accessioned2017-05-08T23:48:34Z
    date available2017-05-08T23:48:34Z
    date copyrightOctober, 1995
    date issued1995
    identifier issn0889-504X
    identifier otherJOTUEI-28646#635_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116120
    description abstractThis paper describes the design, operation, construction, and demonstration of a new type of high-bandwidth unsteady temperature sensor based on fiber optics, and capable of operating in a high-speed multistage research compressor with flow representative of jet engine conditions. The sensing element is an optical coating of zinc selenide deposited on the end of an optical fiber. During evaluation in aerodynamic testing, a 1 K gas temperature resolution was demonstrated at 9.6 kHz and an upper bandwidth limit of 36 kHz achieved.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Fiber Optic Probe for Gas Total Temperature Measurement in Turbomachinery
    typeJournal Paper
    journal volume117
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2836582
    journal fristpage635
    journal lastpage641
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsTemperature
    keywordsFibers
    keywordsTemperature measurement
    keywordsCompressors
    keywordsConstruction
    keywordsOptical coatings
    keywordsResolution (Optics)
    keywordsDesign
    keywordsTesting
    keywordsJet engines
    keywordsOptical fiber
    keywordsProbes
    keywordsTemperature sensors AND Turbomachinery
    treeJournal of Turbomachinery:;1995:;volume( 117 ):;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
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