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Experimental study of flow reattachment in a single-sided sudden expansion

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TLDR
The importance of changing the structure of the separated shear layer on the reattachment process itself was examined in this article, where the authors developed a pulsed wall probe for measurement of skin friction in the re-attachment region, thus providing an unambiguous definition of the Reattachment length.
Abstract
The reattachment of a fully turbulent, two dimensional, separated shear layer downstream of a single-sided sudden expansion in a planar duct flow was examined experimentally. The importance of changing the structure of the separated shear layer on the reattachment process itself was examined. For all cases, the Reynolds number based on step height was greater than 20,000, the expansion ratio was 5/3, and the inlet boundary layer was less than one-half step height in thickness. A crucially important phase was the development of a pulsed wall probe for measurement of skin friction in the reattachment region, thus providing an unambiguous definition of the reattachment length. Quantitative features of reattachment - including streamwise development of the mean and fluctuating velocity field, pressure rise, and skin friction - were found to be similar for all cases studied when scaled by the reattachment length. A definition of the reattachment zone is proposed.

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An experimental investigation of a turbulent shear flow with separation, reverse flow, and reattachment

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The structure of a turbulent shear layer bounding a separation region

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References
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Calibration of the Preston tube and limitations on its use in pressure gradients

TL;DR: In this paper, it is shown that in sufficiently strong favorable and adverse pressure gradients the inner-law velocity distribution breaks down completely, and it is suggested that this breakdown is associated with reversion to laminar flow.
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The flow around a surface-mounted cube in uniform and turbulent streams

TL;DR: In this article, an experimental investigation of the flow around surface mounted cubes in both uniform, irrotational and sheared, turbulent flows is described, and comparisons with the somewhat sparse measurements of previous workers are made and the relevance of recent theoretical attempts to describe the flow, as opposed to numerical calculation techniques to predict it, is briefly discussed.

Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition

TL;DR: In this paper, the results of experimental and theoretical research conducted on flow separation associated with steps, bases, compression corners, curved surfaces, shock-wave boundary-layer reflections, and configurations producing leading-edge separation are presented.
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Investigation of the flow behind a two-dimensional model with a blunt trailing edge and fitted with splitter plates

TL;DR: In this article, the authors examined the flow in the wake of a two-dimensional model with a blunt trailing edge at Reynolds numbers (based on model chord) between 1·4 × 105 and 2·56 × 105.
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The reattachment and relaxation of a turbulent shear layer

TL;DR: In this article, the authors show that the splitting of the shear layer at reattachment, where part of the flow is deflected upstream into the recirculating flow region to supply the entrainment, causes a pronounced decrease in eddy length scale, evidently because the larger eddies are torn in two.
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