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contributor authorRonald J. Chila
contributor authorDeborah A. Kaminski
date accessioned2017-05-09T00:28:16Z
date available2017-05-09T00:28:16Z
date copyrightDecember, 2008
date issued2008
identifier issn0098-2202
identifier otherJFEGA4-27349#121403_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/138130
description abstractGrid independence is frequently an overlooked item in computational fluid dynamics (CFD) analyses. Results obtained from grid dependent solutions may prove to be costly, in that engineering design decisions can be made using potentially faulty information. An automated method for grid independence is developed for two-dimensional unstructured wall function grids. Grid independence is achieved via successive levels of adaptive refinement. Adaptive refinement is performed in an automated manner and is based on multiple field variables. Sensors are placed at strategic locations within the flow field, which are determined by examining the CFD solution of a uniform grid. Three cases are examined, the backward-facing step, flow over an asymmetric transonic airfoil, and hydrogen combustion in a channel. Grid independent solutions are obtained for all three cases. Results for each case compare well with experimental data and/or other numerical predictions.
publisherThe American Society of Mechanical Engineers (ASME)
titleGrid Independence Via Automated Unstructured Adaptation
typeJournal Paper
journal volume130
journal issue12
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3001099
journal fristpage121403
identifier eissn1528-901X
keywordsCombustion
keywordsChannels (Hydraulic engineering)
keywordsSensors
keywordsFoundry coatings
keywordsComputational fluid dynamics
keywordsCycles
keywordsErrors
keywordsAirfoils
keywordsHydrogen AND Flow (Dynamics)
treeJournal of Fluids Engineering:;2008:;volume( 130 ):;issue: 012
contenttypeFulltext


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