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    Reynolds Stresses and Dissipation Mechanisms Downstream of a Turbine Cascade

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 002::page 258
    Author:
    J. Moore
    ,
    D. M. Shaffer
    ,
    J. G. Moore
    DOI: 10.1115/1.3262096
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation was performed to measure Reynolds stresses in the turbulent flow downstream of a large-scale linear turbine cascade. A rotatable X-wire hot-wire probe that allows redundant data to be taken with solution for mean velocities and turbulence quantities by least-squares fitting procedures was developed. The rotatable X-wire was used to obtain the Reynolds stresses on a measurement plane located 10 percent of an axial chord downstream of the trailing edge. Here the turbulence kinetic energy exhibits a distribution resembling the contours of total pressure loss obtained previously, but is highest in the blade wake where losses are relatively low. The turbulent shear stresses obtained are consistent in sign and magnitude with the gradients of mean velocity. The measured Reynolds stresses are combined with measured distributions of velocity to show how and where losses are being produced. The mechanisms for the dissipation of mean kinetic energy in this swirling three-dimensional flow are revealed.
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      Reynolds Stresses and Dissipation Mechanisms Downstream of a Turbine Cascade

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    https://yetl.yabesh.ir/yetl1/handle/yetl/103248
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    contributor authorJ. Moore
    contributor authorD. M. Shaffer
    contributor authorJ. G. Moore
    date accessioned2017-05-08T23:26:04Z
    date available2017-05-08T23:26:04Z
    date copyrightApril, 1987
    date issued1987
    identifier issn0889-504X
    identifier otherJOTUEI-28583#258_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103248
    description abstractAn experimental investigation was performed to measure Reynolds stresses in the turbulent flow downstream of a large-scale linear turbine cascade. A rotatable X-wire hot-wire probe that allows redundant data to be taken with solution for mean velocities and turbulence quantities by least-squares fitting procedures was developed. The rotatable X-wire was used to obtain the Reynolds stresses on a measurement plane located 10 percent of an axial chord downstream of the trailing edge. Here the turbulence kinetic energy exhibits a distribution resembling the contours of total pressure loss obtained previously, but is highest in the blade wake where losses are relatively low. The turbulent shear stresses obtained are consistent in sign and magnitude with the gradients of mean velocity. The measured Reynolds stresses are combined with measured distributions of velocity to show how and where losses are being produced. The mechanisms for the dissipation of mean kinetic energy in this swirling three-dimensional flow are revealed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleReynolds Stresses and Dissipation Mechanisms Downstream of a Turbine Cascade
    typeJournal Paper
    journal volume109
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3262096
    journal fristpage258
    journal lastpage267
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;1987:;volume( 109 ):;issue: 002
    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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