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    Coriolis Effects on the Flow Field Inside a Rotating Triangular Channel for Leading Edge Cooling

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 003::page 31019
    Author:
    Pascotto, Matteo
    ,
    Armellini, Alessandro
    ,
    Mucignat, Claudio
    ,
    Casarsa, Luca
    DOI: 10.1115/1.4025570
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The flow field inside a rotating smooth radial channel with a triangular shaped cross section is investigated. Test conditions resemble those pertaining to the passages used for the internal cooling of the gas turbine blade's leading edge. Heat transfer data are also available from the literature on the same geometry and at comparable working conditions and have been profitably used for a combined aerothermal analysis. The model consists of a straight smooth channel with an equilateral triangle cross section. The rotation axis is aligned with one of the triangle bisectors. Two dimensional particle image velocimetry (PIV) and stereoPIV were used in order to characterize the inlet flow (in static conditions) and the rotationinduced secondary flow in the channel cross section at Re = 20,000, Ro = 0.2 and Re = 10,000, Ro = 0.4. A wider range of working conditions (Re = 10,000–40,000, Ro = 0.2–0.6) was explored by means of Reynolds averaged Navier–Stokes (RANS) simulations carefully validated by the available PIV data. The turbulence was modeled by means of the shear stress transport (SST) model with a hybrid nearwall treatment. The results show that the rotationinduced flow structure is rather complicated and show relevant differences compared to the flow models that have been considered thus far. Indeed, the secondary flow turned out to be characterized by the presence of two or more vortex cells, depending on channel location and Ro number. No separation or reattachment of these structures is found on the channel walls but they have been observed at the channel apexes. The streamwise velocity distribution shows a velocity peak close to the lower apex and the overall flow structure does not reach a steady configuration along the channel length. This evolution is fastened (in space) if the rotation number is increased while changes of the Re number have no effect. Finally, due to the understanding of the flow mechanisms associated with rotation, it was possible to provide a precise justification of the channel thermal behavior.
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      Coriolis Effects on the Flow Field Inside a Rotating Triangular Channel for Leading Edge Cooling

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    contributor authorPascotto, Matteo
    contributor authorArmellini, Alessandro
    contributor authorMucignat, Claudio
    contributor authorCasarsa, Luca
    date accessioned2017-05-09T01:13:32Z
    date available2017-05-09T01:13:32Z
    date issued2014
    identifier issn0889-504X
    identifier otherturbo_136_03_031019.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/156581
    description abstractThe flow field inside a rotating smooth radial channel with a triangular shaped cross section is investigated. Test conditions resemble those pertaining to the passages used for the internal cooling of the gas turbine blade's leading edge. Heat transfer data are also available from the literature on the same geometry and at comparable working conditions and have been profitably used for a combined aerothermal analysis. The model consists of a straight smooth channel with an equilateral triangle cross section. The rotation axis is aligned with one of the triangle bisectors. Two dimensional particle image velocimetry (PIV) and stereoPIV were used in order to characterize the inlet flow (in static conditions) and the rotationinduced secondary flow in the channel cross section at Re = 20,000, Ro = 0.2 and Re = 10,000, Ro = 0.4. A wider range of working conditions (Re = 10,000–40,000, Ro = 0.2–0.6) was explored by means of Reynolds averaged Navier–Stokes (RANS) simulations carefully validated by the available PIV data. The turbulence was modeled by means of the shear stress transport (SST) model with a hybrid nearwall treatment. The results show that the rotationinduced flow structure is rather complicated and show relevant differences compared to the flow models that have been considered thus far. Indeed, the secondary flow turned out to be characterized by the presence of two or more vortex cells, depending on channel location and Ro number. No separation or reattachment of these structures is found on the channel walls but they have been observed at the channel apexes. The streamwise velocity distribution shows a velocity peak close to the lower apex and the overall flow structure does not reach a steady configuration along the channel length. This evolution is fastened (in space) if the rotation number is increased while changes of the Re number have no effect. Finally, due to the understanding of the flow mechanisms associated with rotation, it was possible to provide a precise justification of the channel thermal behavior.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCoriolis Effects on the Flow Field Inside a Rotating Triangular Channel for Leading Edge Cooling
    typeJournal Paper
    journal volume136
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4025570
    journal fristpage31019
    journal lastpage31019
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2014:;volume( 136 ):;issue: 003
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian