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contributor authorJ. U. Schlüter
contributor authorX. Wu
contributor authorS. Kim
contributor authorS. Shankaran
contributor authorJ. J. Alonso
contributor authorH. Pitsch
date accessioned2017-05-09T00:16:32Z
date available2017-05-09T00:16:32Z
date copyrightJuly, 2005
date issued2005
identifier issn0098-2202
identifier otherJFEGA4-27210#806_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/131995
description abstractFull-scale numerical prediction of the aerothermal flow in gas turbine engines are currently limited by high computational costs. The approach presented here intends the use of different specialized flow solvers based on the Reynolds-averaged Navier-Stokes equations as well as large-eddy simulations for different parts of the flow domain, running simultaneously and exchanging information at the interfaces. This study documents the development of the interface and proves its accuracy and efficiency with simple test cases. Furthermore, its application to a turbomachinery application is demonstrated.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Framework for Coupling Reynolds-Averaged With Large-Eddy Simulations for Gas Turbine Applications
typeJournal Paper
journal volume127
journal issue4
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.1994877
journal fristpage806
journal lastpage815
identifier eissn1528-901X
keywordsFlow (Dynamics)
keywordsBoundary-value problems
keywordsReynolds-averaged Navier–Stokes equations AND Computation
treeJournal of Fluids Engineering:;2005:;volume( 127 ):;issue: 004
contenttypeFulltext


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