scispace - formally typeset
Search or ask a question
Topic

Flow separation

About: Flow separation is a research topic. Over the lifetime, 16708 publications have been published within this topic receiving 386926 citations.


Papers
More filters
Journal ArticleDOI
TL;DR: In this paper, a methodology was devised for the design of three-dimensional hypersonic Inlets, which makes extensive use of inviscid stream-tracing techniques to generate an inlet with smooth shape transition from a rectangular-like capture to an elliptical throat.
Abstract: A methodology has been devised for the design of three-dimensional hypersonic Inlets, This methodology makes extensive use of inviscid stream-tracing techniques to generate an inlet with smooth shape transition from a rectangular-like capture to an elliptical throat. Highly swept leading edges and a significantly notched cowl enable use of these inlets in fixed geometry configurations. The design procedure includes a three-dimensional viscous correction and uses established correlations to check for boundary-layer separation caused by shock wave interactions. Complete details of the design procedure are presented and the characteristics of a modular inlet with a design point of Mach 6.0 are examined. Comparison with a classical two-dimensional inlet optimized for maximum total pressure recovery indicates that these three-dimensional inlets demonstrate good inviscid performance even when operating well below the design point. An estimate of the on-design viscous performance corresponds with that of an efficient inlet for scramjet applications.

224 citations

Journal ArticleDOI
TL;DR: In this paper, the authors measured mean velocity, Reynolds-shear-stress and Reynolds-normal-stress distributions of highly turbulent and disturbed flow over a bluff plate with a long splitter plate in its plane of symmetry.
Abstract: Experiments were performed in the highly turbulent and disturbed flow over a bluff plate with a long splitter plate in its plane of symmetry. The flow separates at the sharp bevelled edge of the bluff plate, forms a free shear layer on top of the reverse-flow region which is bounded on its other side by the splitter plate, and reattaches on the splitter plate over a narrow region curved in spanwise direction. Downstream of reattachment the shear flow adjusts slowly to the wall boundary conditions. Measurements of mean velocity, Reynolds-shear-stress and Reynolds-normal-stress distributions were carried out by hot-wire and pulsed-wire anemometry. The latter technique was used in those regions of the flow where reverse flow occurred or where the flow was highly turbulent. Spectra and integral lengthscales were measured to investigate the state and structure of the flow. The large-eddy structure in the inner region of the flow had lengthscales in the two cross-stream directions which were approximately equal, indicating a fast break-up of spanwise structures just downstream from separation. Mean and fluctuating quantities showed a self-similar behaviour in a short region upstream of reattachment and ‘profile similarity’ in the separated shear layer and along the splitter plate downstream from reattachment. Probability-density distributions of skin friction were measured and used to calculate mean and fluctuating values. No flapping of the reattaching shear layer could be observed. Pulsed-wire measurements revealed that the logarithmic law of the wall does not hold either in the reverse-flow region or in a region about half the length of the bubble downstream from reattachment.

224 citations

01 Dec 1964
TL;DR: A brief review of the literature on turbulent flow of high-polymer solutions is given in this article, where the authors show that the maximum drag reduction achievable by polymer addition appears to be a function of the Reynolds number of the flow.
Abstract: : A brief review is given of the literature on turbulent flow of high- polymer solutions Laboratory experiments using rotating disks and turbulent pipe flow have led to generalizations as to characteristics of friction-reducing high polymers Linear, high-molecular-weight, soluble polymers are shown to be most effective The maximum drag reduction achievable by polymer addition appears to be a function of the Reynolds number of the flow

222 citations

Debra Spinks1
01 Dec 1997
TL;DR: The 1997 annual progress reports of the research fellows and students supported by the Center for Turbulence Research (CTR) as discussed by the authors show that large-eddy simulation of turbulent mixing has been successfully applied to high-lift airfoils.
Abstract: This report contains the 1997 annual progress reports of the research fellows and students supported by the Center for Turbulence Research (CTR). Titles include: Invariant modeling in large-eddy simulation of turbulence; Validation of large-eddy simulation in a plain asymmetric diffuser; Progress in large-eddy simulation of trailing-edge turbulence and aeronautics; Resolution requirements in large-eddy simulations of shear flows; A general theory of discrete filtering for LES in complex geometry; On the use of discrete filters for large eddy simulation; Wall models in large eddy simulation of separated flow; Perspectives for ensemble average LES; Anisotropic grid-based formulas for subgrid-scale models; Some modeling requirements for wall models in large eddy simulation; Numerical simulation of 3D turbulent boundary layers using the V2F model; Accurate modeling of impinging jet heat transfer; Application of turbulence models to high-lift airfoils; Advances in structure-based turbulence modeling; Incorporating realistic chemistry into direct numerical simulations of turbulent non-premixed combustion; Effects of small-scale structure on turbulent mixing; Turbulent premixed combustion in the laminar flamelet and the thin reaction zone regime; Large eddy simulation of combustion instabilities in turbulent premixed burners; On the generation of vorticity at a free-surface; Active control of turbulent channel flow; A generalized framework for robust control in fluid mechanics; Combined immersed-boundary/B-spline methods for simulations of flow in complex geometries; and DNS of shock boundary-layer interaction - preliminary results for compression ramp flow.

222 citations

Journal ArticleDOI
TL;DR: In this article, a model for aerodynamic lift of wind turbine profiles under dynamic stall conditions is presented, where the model combines memory delay effects under attached flow with reduced lift due to flow separation.

221 citations


Network Information
Related Topics (5)
Reynolds number
68.4K papers, 1.6M citations
94% related
Laminar flow
56K papers, 1.2M citations
91% related
Boundary layer
64.9K papers, 1.4M citations
91% related
Turbulence
112.1K papers, 2.7M citations
88% related
Vortex
72.3K papers, 1.3M citations
86% related
Performance
Metrics
No. of papers in the topic in previous years
YearPapers
2023177
2022333
2021361
2020394
2019403
2018371