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contributor authorJohn A. Redford
contributor authorMark W. Johnson
date accessioned2017-05-09T00:18:07Z
date available2017-05-09T00:18:07Z
date copyrightJuly, 2005
date issued2005
identifier issn0889-504X
identifier otherJOTUEI-28721#497_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/132787
description abstractThis paper describes the modifications made to a successful attached flow transition model to produce a model capable of predicting both attached and separated flow transition. This transition model is used in combination with the Fluent CFD software, which is used to compute the flow around the blade assuming that it remains entirely laminar. The transition model then determines the start of transition location and the development of the intermittency. These intermittency values weight the laminar and turbulent boundary layer profiles to obtain the resulting transitional boundary layer parameters. The ERCOFTAC T3L test cases are used to validate the predictions. The T3L blade is a flat plate with a semi-circular leading edge, which results in the formation of a separation bubble the length of which is strongly dependent on the transition process. Predictions were performed for five T3L test cases for differing free-stream turbulence levels and Reynolds numbers. For the majority of these test cases the measurements were accurately predicted.
publisherThe American Society of Mechanical Engineers (ASME)
titlePredicting Transitional Separation Bubbles
typeJournal Paper
journal volume127
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1860573
journal fristpage497
journal lastpage501
identifier eissn1528-8900
keywordsFlow (Dynamics)
keywordsSeparation (Technology)
keywordsTurbulence
keywordsBubbles
keywordsBoundary layers AND Reynolds number
treeJournal of Turbomachinery:;2005:;volume( 127 ):;issue: 003
contenttypeFulltext


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