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    The Effects of the Vane and Mainstream Turbulence Level on Hot Streak Attenuation

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 001::page 215
    Author:
    Sean C. Jenkins
    ,
    David G. Bogard
    DOI: 10.1115/1.1812777
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper discusses the effects of varying pitch position on the attenuation of a simulated hot streak in a vane cascade under conditions of low and high turbulence. Measurements describe the effect of both small and large changes in pitch away from the stagnation line as evidenced by hot streak variations in the wake and at the trailing edge. Under both turbulence conditions, the vane serves to increase or decrease the attenuation rate depending on the location of the hot streak relative to the vane due to isolating of the hot streak core by the vane wall. Additional attenuation resulted due to the action of the wake on the hot streak.
    keyword(s): Turbulence , Suction , Wakes , Pressure , Temperature , Measurement AND Temperature gradients ,
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      The Effects of the Vane and Mainstream Turbulence Level on Hot Streak Attenuation

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    http://yetl.yabesh.ir/yetl1/handle/yetl/132854
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    contributor authorSean C. Jenkins
    contributor authorDavid G. Bogard
    date accessioned2017-05-09T00:18:18Z
    date available2017-05-09T00:18:18Z
    date copyrightJanuary, 2005
    date issued2005
    identifier issn0889-504X
    identifier otherJOTUEI-28717#215_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/132854
    description abstractThis paper discusses the effects of varying pitch position on the attenuation of a simulated hot streak in a vane cascade under conditions of low and high turbulence. Measurements describe the effect of both small and large changes in pitch away from the stagnation line as evidenced by hot streak variations in the wake and at the trailing edge. Under both turbulence conditions, the vane serves to increase or decrease the attenuation rate depending on the location of the hot streak relative to the vane due to isolating of the hot streak core by the vane wall. Additional attenuation resulted due to the action of the wake on the hot streak.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Effects of the Vane and Mainstream Turbulence Level on Hot Streak Attenuation
    typeJournal Paper
    journal volume127
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1812777
    journal fristpage215
    journal lastpage221
    identifier eissn1528-8900
    keywordsTurbulence
    keywordsSuction
    keywordsWakes
    keywordsPressure
    keywordsTemperature
    keywordsMeasurement AND Temperature gradients
    treeJournal of Turbomachinery:;2005:;volume( 127 ):;issue: 001
    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