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    The Unsteady Development of a Turbulent Wake Through a Downstream Low-Pressure Turbine Blade Passage

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 002::page 388
    Author:
    R. D. Stieger
    ,
    H. P. Hodson
    DOI: 10.1115/1.1811094
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents two-dimensional LDA measurements of the convection of a wake through a low-pressure turbine cascade. Previous studies have shown the wake convection to be kinematic, but have not provided details of the turbulent field. The spatial resolution of these measurements has facilitated the calculation of the production of turbulent kinetic energy, and this has revealed a mechanism for turbulence production as the wake convects through the blade row. The measured ensemble-averaged velocity field confirmed the previously reported kinematics of wake convection while the measurements of the turbulence quantities showed the wake fluid to be characterized by elevated levels of turbulent kinetic energy (TKE) and to have an anisotropic structure. Based on the measured mean and turbulence quantities, the production of turbulent kinetic energy was calculated. This highlighted a TKE production mechanism that resulted in increased levels of turbulence over the rear suction surface where boundary-layer transition occurs. The turbulence production mechanism within the blade row was also observed to produce more anisotropic turbulence. Production occurs when the principal stresses within the wake are aligned with the mean strains. This coincides with the maximum distortion of the wake within the blade passage and provides a mechanism for the production of turbulence outside of the boundary layer.
    keyword(s): Pressure , Flow (Dynamics) , Fluids , Measurement , Turbulence , Stress , Wakes , Convection , Blades , Turbine blades , Suction , Wake turbulence , Boundary layers AND Cascades (Fluid dynamics) ,
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      The Unsteady Development of a Turbulent Wake Through a Downstream Low-Pressure Turbine Blade Passage

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    https://yetl.yabesh.ir/yetl1/handle/yetl/132825
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    contributor authorR. D. Stieger
    contributor authorH. P. Hodson
    date accessioned2017-05-09T00:18:13Z
    date available2017-05-09T00:18:13Z
    date copyrightApril, 2005
    date issued2005
    identifier issn0889-504X
    identifier otherJOTUEI-28719#388_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/132825
    description abstractThis paper presents two-dimensional LDA measurements of the convection of a wake through a low-pressure turbine cascade. Previous studies have shown the wake convection to be kinematic, but have not provided details of the turbulent field. The spatial resolution of these measurements has facilitated the calculation of the production of turbulent kinetic energy, and this has revealed a mechanism for turbulence production as the wake convects through the blade row. The measured ensemble-averaged velocity field confirmed the previously reported kinematics of wake convection while the measurements of the turbulence quantities showed the wake fluid to be characterized by elevated levels of turbulent kinetic energy (TKE) and to have an anisotropic structure. Based on the measured mean and turbulence quantities, the production of turbulent kinetic energy was calculated. This highlighted a TKE production mechanism that resulted in increased levels of turbulence over the rear suction surface where boundary-layer transition occurs. The turbulence production mechanism within the blade row was also observed to produce more anisotropic turbulence. Production occurs when the principal stresses within the wake are aligned with the mean strains. This coincides with the maximum distortion of the wake within the blade passage and provides a mechanism for the production of turbulence outside of the boundary layer.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Unsteady Development of a Turbulent Wake Through a Downstream Low-Pressure Turbine Blade Passage
    typeJournal Paper
    journal volume127
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1811094
    journal fristpage388
    journal lastpage394
    identifier eissn1528-8900
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsFluids
    keywordsMeasurement
    keywordsTurbulence
    keywordsStress
    keywordsWakes
    keywordsConvection
    keywordsBlades
    keywordsTurbine blades
    keywordsSuction
    keywordsWake turbulence
    keywordsBoundary layers AND Cascades (Fluid dynamics)
    treeJournal of Turbomachinery:;2005:;volume( 127 ):;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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