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    Large Eddy Simulation for Turbines: Methodologies, Cost and Future Outlooks

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 006::page 61009
    Author:
    Tyacke, James
    ,
    Tucker, Paul
    ,
    Jefferson
    ,
    Rao Vadlamani, Nagabushana
    ,
    Watson, Robert
    ,
    Naqavi, Iftekhar
    ,
    Yang, Xiaoyu
    DOI: 10.1115/1.4025589
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Flows throughout different zones of turbines have been investigated using large eddy simulation (LES) and hybrid Reynoldsaveraged Navier–StokesLES (RANSLES) methods and contrasted with RANS modeling, which is more typically used in the design environment. The studied cases include low and highpressure turbine cascades, real surface roughness effects, internal cooling ducts, trailing edge cutbacks, and labyrinth and rim seals. Evidence is presented that shows that LES and hybrid RANSLES produces higher quality data than RANS/URANS for a wide range of flows. The higher level of physics that is resolved allows for greater flow physics insight, which is valuable for improving designs and refining lower order models. Turbine zones are categorized by flow type to assist in choosing the appropriate eddy resolving method and to estimate the computational cost.
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      Large Eddy Simulation for Turbines: Methodologies, Cost and Future Outlooks

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    contributor authorTyacke, James
    contributor authorTucker, Paul
    contributor authorJefferson
    contributor authorRao Vadlamani, Nagabushana
    contributor authorWatson, Robert
    contributor authorNaqavi, Iftekhar
    contributor authorYang, Xiaoyu
    date accessioned2017-05-09T01:13:38Z
    date available2017-05-09T01:13:38Z
    date issued2014
    identifier issn0889-504X
    identifier otherturbo_136_06_061009.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/156610
    description abstractFlows throughout different zones of turbines have been investigated using large eddy simulation (LES) and hybrid Reynoldsaveraged Navier–StokesLES (RANSLES) methods and contrasted with RANS modeling, which is more typically used in the design environment. The studied cases include low and highpressure turbine cascades, real surface roughness effects, internal cooling ducts, trailing edge cutbacks, and labyrinth and rim seals. Evidence is presented that shows that LES and hybrid RANSLES produces higher quality data than RANS/URANS for a wide range of flows. The higher level of physics that is resolved allows for greater flow physics insight, which is valuable for improving designs and refining lower order models. Turbine zones are categorized by flow type to assist in choosing the appropriate eddy resolving method and to estimate the computational cost.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLarge Eddy Simulation for Turbines: Methodologies, Cost and Future Outlooks
    typeJournal Paper
    journal volume136
    journal issue6
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4025589
    journal fristpage61009
    journal lastpage61009
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2014:;volume( 136 ):;issue: 006
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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