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contributor authorF. Durst
contributor authorJ. C. F. Pereira
date accessioned2017-05-08T23:27:26Z
date available2017-05-08T23:27:26Z
date copyrightSeptember, 1988
date issued1988
identifier issn0098-2202
identifier otherJFEGA4-27036#289_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/104040
description abstractThis paper presents results of numerical studies of the impulsively starting backward-facing step flow with the step being mounted in a plane, two-dimensional duct. Results are presented for Reynolds numbers of Re = 10; 368 and 648 and for the last two Reynolds numbers comparisons are given between experimental and numerical results obtained for the final steady state flow conditions. In the computational scheme, the convective terms in the momentum equations are approximated by a 13-point quadratic upstream weighted finite-difference scheme and a fully implicit first order forward differencing scheme is used to discretize the temporal derivatives. The computations show that for the higher Reynolds numbers, the flow starts to separate on the lower and upper corners of the step yielding two disconnected recirculating flow regions for some time after the flow has been impulsively started. As time progresses, these two separated flow regions connect up and a single recirculating flow region emerges. This separated flow region stays attached to the step, grows in size and approaches, for the time t → ∞, the dimensions measured and predicted for the separation region for steady laminar backward-facing flow. For the Reynolds number Re = 10 the separation starts at the bottom of the backward-facing step and the separation region enlarges with time until the steady state flow pattern is reached. At the channel wall opposite to the step and for Reynolds number Re = 368, a separated flow region is observed and it is shown to occur for some finite time period of the developing, impulsively started backward-facing step flow. Its dimensions change with time and reduce to zero before the steady state flow pattern is reached. For the higher Reynolds number Re = 648, the secondary separated flow region opposite to the wall is also present and it is shown to remain present for t → ∞. Two kinds of the inlet conditions were considered; the inlet mean flow was assumed to be constant in a first study and was assumed to increase with time in a second one. The predicted flow field for t → ∞ turned out to be identical for both cases. They were also identical to the flow field predicted for steady, backward-facing step flow using the same numerical grid as for the time-dependent predictions.
publisherThe American Society of Mechanical Engineers (ASME)
titleTime-Dependent Laminar Backward-Facing Step Flow in a Two-Dimensional Duct
typeJournal Paper
journal volume110
journal issue3
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3243547
journal fristpage289
journal lastpage296
identifier eissn1528-901X
keywordsFlow (Dynamics)
keywordsFoundry coatings
keywordsDucts
keywordsReynolds number
keywordsSteady state
keywordsSeparation (Technology)
keywordsDimensions
keywordsMomentum
keywordsChannels (Hydraulic engineering)
keywordsEquations
keywordsCorners (Structural elements) AND Computation
treeJournal of Fluids Engineering:;1988:;volume( 110 ):;issue: 003
contenttypeFulltext


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