Large Eddy Simulation for Turbines: Methodologies, Cost and Future OutlooksSource: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 006::page 61009Author:Tyacke, James
,
Tucker, Paul
,
Jefferson
,
Rao Vadlamani, Nagabushana
,
Watson, Robert
,
Naqavi, Iftekhar
,
Yang, Xiaoyu
DOI: 10.1115/1.4025589Publisher: 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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| contributor author | Tyacke, James | |
| contributor author | Tucker, Paul | |
| contributor author | Jefferson | |
| contributor author | Rao Vadlamani, Nagabushana | |
| contributor author | Watson, Robert | |
| contributor author | Naqavi, Iftekhar | |
| contributor author | Yang, Xiaoyu | |
| date accessioned | 2017-05-09T01:13:38Z | |
| date available | 2017-05-09T01:13:38Z | |
| date issued | 2014 | |
| identifier issn | 0889-504X | |
| identifier other | turbo_136_06_061009.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/156610 | |
| description 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. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Large Eddy Simulation for Turbines: Methodologies, Cost and Future Outlooks | |
| type | Journal Paper | |
| journal volume | 136 | |
| journal issue | 6 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.4025589 | |
| journal fristpage | 61009 | |
| journal lastpage | 61009 | |
| identifier eissn | 1528-8900 | |
| tree | Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 006 | |
| contenttype | Fulltext |