Show simple item record

contributor authorDragan Kožulović
contributor authorB. Leigh Lapworth
date accessioned2017-05-09T00:35:48Z
date available2017-05-09T00:35:48Z
date copyrightJuly, 2009
date issued2009
identifier issn0889-504X
identifier otherJOTUEI-28755#031008_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142162
description abstractThe implementation of an integral transition model in a parallel unstructured computational fluid dynamics code is described. In particular, an algorithm for gathering the nonlocal boundary layer values (momentum thickness and shape factor) from parallel distributed computational domains is presented. Transition modeling results are presented for a flat plate and for a low pressure turbine, covering a large variation of Reynolds numbers, Mach numbers, turbulence intensities, and incidence angles. Contrary to fully turbulent simulations, transitional predictions are in very good agreement with measurements. Furthermore, the computational overhead of transitional simulations is only 7% for one multigrid cycle.
publisherThe American Society of Mechanical Engineers (ASME)
titleAn Approach for Inclusion of a Nonlocal Transition Model in a Parallel Unstructured Computational Fluid Dynamics Code
typeJournal Paper
journal volume131
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2987238
journal fristpage31008
identifier eissn1528-8900
keywordsPressure
keywordsBoundary layers
keywordsComputational fluid dynamics
keywordsEngineering simulation
keywordsModeling
keywordsTurbulence
keywordsReynolds number
keywordsFlow (Dynamics)
keywordsMach number
keywordsTurbines
keywordsAlgorithms
keywordsMeasurement
keywordsSeparation (Technology)
keywordsMomentum
keywordsCycles
keywordsThickness AND Flat plates
treeJournal of Turbomachinery:;2009:;volume( 131 ):;issue: 003
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record