1974
DOI: 10.1017/s0022112074002035
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Low Reynolds number flow over a plane symmetric sudden expansion

Abstract: Flow visualization and laser-anemometry measurements are reported in the flow downstream of a plane 3: 1 symmetric expansion in a duct with an aspect ratio of 9·2: 1 downstream of the expansion. The flow was found to be markedly dependent on Reynolds number, and strongly three-dimensional even well away from the channel corners except at the lowest measurable velocities. The measurements at a Reynolds number of 56 indicated that the separation regions behind each step were of equal length. Symmetric velocity p… Show more

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Cited by 285 publications
(167 citation statements)
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“…Experimental results show that, for low Re, the flow is symmetric about the channel centerline, with circulation regions formed at the corners of the expansion (Durst et al 1973). This is the case depicted in figure 6, in which the flow is described by streamlines.…”
Section: ) Description Of Experimentsmentioning
confidence: 75%
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“…Experimental results show that, for low Re, the flow is symmetric about the channel centerline, with circulation regions formed at the corners of the expansion (Durst et al 1973). This is the case depicted in figure 6, in which the flow is described by streamlines.…”
Section: ) Description Of Experimentsmentioning
confidence: 75%
“…Specifically, we consider two-dimensional Sudden Expansion flows. In fluid dynamics, such flows have been of considerable interest (Durst et al 1973;Cherdron et al 1978;Fearn et al 1990) and continue to do so. Due to the breaking of symmetries with increasing Reynolds number and the consequent development of at least bimodal statistics, it provides a test case particularly well-suited to the evaluation of data assimilation schemes.…”
Section: B Sudden Expansion Flowsmentioning
confidence: 99%
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“…For low Re, the flow remains steady and symmetric about the centerline, with recirculation zones appearing at the corners of the expansion (Durst et al 1974). At larger Re, the flow downstream of the expansion develops asymmetry and exhibits vortex shedding, which can either be steady or unsteady.…”
Section: A Experimental Setup and Test Proceduresmentioning
confidence: 99%
“…Due to the very long downstream channel (300H), the gradient of flow variables at the outlet is null, except for the pressure that is linearly extrapolated from the domain. This benchmark problem has been extensively used to verify numerical solutions and schemes [33,34,35] used in incompressible laminar flow of Newtonian and non-Newtonian fluids. At low Reynolds numbers the flow is symmetric and at a critical Reynolds number, that depends on expansion ratio, the flow becomes asymmetric [34], but remains steady.…”
Section: Sudden Expansionmentioning
confidence: 99%