An Experimental Investigation of a Two-dimensional Turbulent Jet Flow Over a Rotating Cylinder PDF Download
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Author: Helmut Keil
Publisher:
ISBN:
Category :
Languages : en
Pages : 130
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Author: Helmut Keil
Publisher:
ISBN:
Category :
Languages : en
Pages : 130
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Author: David Charles Thoman
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Category :
Languages : en
Pages : 178
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Author: Kombupalayam Malayanan Kumaravel Prakash
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Category :
Languages : en
Pages : 356
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Author: Jackson Lee Nelson
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Category :
Languages : en
Pages : 160
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Author: Han-Lieh Liu
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Category :
Languages : en
Pages : 326
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Author: Julien Rémy Dominique Gérard Landel
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Category :
Languages : en
Pages :
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The study of quasi-two-dimensional turbulent jets is relevant to chemical reactors, the coking process in oil refinement, as well as rivers flowing into lakes or oceans. In the event of a spillage of pollutants into a river, it is critical to understand how these agents disperse with the flow in order to assess damage to the environment. For such flows, characteristic streamwise and cross-stream dimensions can be much larger than the fluid-layer thickness, and so the flow develops in a confined environment. When the distance away from the discharge location is larger than ten times the fluid-layer thickness, the flow is referred to as a quasi-two-dimensional jet. From experimental observations using dyed jets and particle image velocimetry, we find that the structure of a quasi-two-dimensional jet consists of a high-speed meandering core with large counter-rotating eddies developing on alternate sides of the core. The core and eddy structure is self-similar with distance from the discharge location. The Gaussianity of the cross-stream distribution of the time-averaged velocity is due, in part, to the sinuous instability of the core. To understand the transport and dispersion properties of quasi-two-dimensional jets we use a time-dependent advection--diffusion equation, with a mixing length hypothesis accounting for the turbulent eddy diffusivity. The model is supported by experimental releases of dye in jets or numerical releases of virtual passive tracers in experimentally-measured jet velocity fields. We consider the statistical properties of this flow by releasing and then tracking large clusters of virtual particles in the jet velocity field. The probability distributions of two-point properties (such as the distance between two particles) reveal large streamwise dispersion. Owing to this streamwise dispersive effect, a significant amount of tracers can be transported faster than the speed predicted by a simple advection model. Using potential theory, we determine the flow induced by a quasi-two-dimensional jet confined in a rectangular domain. The streamlines of the induced flow predicted by the theory agree with experimental measurements away from the jet boundary. Finally, we investigate the case of a quasi-two-dimensional particle-laden jet. Depending on the bulk concentration of dense particles, we identify different flow regimes. At low concentrations, the jet features the same core and eddy structure observed without the particles, and thus quasi-two-dimensional jet theory can apply to some extent. At larger concentrations, we observe an oscillating instability of the particle-laden jet.
Author: Young-Min Shim
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 119
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An experimental study was performed for the developing structural characteristics of a plane jet at Re = 3,000. The velocity field measurements were made using particle image velocimetry (PIV) in a water jet facility. The proper orthogonal decomposition (POD) method was applied to the two-dimensional PIV data to reveal large-scale vortical structures in the jet flow. The symmetrical counter-rotating vortices that have been discussed in previous jet studies were confirmed in the initial region. It was found that these vortices were generated as a result of the first vortex merging at the subharmonic sideband frequency, f0 ±fc /2, where f0 was the initial jet shear instability frequency and was the jet column frequency. Moving downstream, their characteristic frequency evolved into f0/2-3fc /4 through nonlinear interaction. In the interaction region, symmetrical vortices were gradually displaced with each other in the streamwise direction and antisymmetrical vortices were eventually formed. The negative correlation between streamwise velocity fluctuations at two points on opposite sides of the jet centreline was caused by the passage of vortical structures. An experimental study was also conducted for the structural characteristics of an impinging jet on a circular cylinder for two cases D/h = 0.5 and 1 where D was the diameter of the cylinder and h was the nozzle height. The mean and turbulent flow fields of the D/h = 0.5 case appeared to be the replica of the wake behind the circular cylinder in cross flow. In contrast, those of the D/h = 1 case showed significantly different features. The alternate vortex shedding and the symmetrical secondary vortices were commonly found in the results of both cases, but the former was pronounced for D/h = 0.5 and the latter was dominant for D/h = 1. The characteristic frequency of the free jet vortices was found to be f0/2 -1/5(f0/2) ; namely, the subharmonic of the initial jet shear layer instability f0 was modulated at 1/5(f0/2. This modulating frequency arose from the upstream propagation of perturbation at the cylinder surface by the impinging free jet vortices. As the free jet vortices approached the cylinder, thin vortex layers were generated due to the adverse pressure gradient. The separation of these vortex layers led to shedding of the symmetrical secondary vortices. The presence of symmetrical secondary vortices instead of alternate vortex shedding suggests a strong influence of the symmetrically arranged free jet vortices. For D/h = 0.5, the free jet vortices and the symmetrical secondary vortices interacted convectively as they moved downstream parallel to the centreline of the flow field. As a result, the alternate vortex shedding was formed and the corresponding frequency spectra exhibited multiple peaks at discrete frequencies. For D/h = 1, the symmetrical secondary vortices were convected downstream without a direct interaction with the free jet vortices due to the deflection of the free jet vortices away from the cylinder. The alternate vortex shedding was also observed but its characteristic frequency was much lower than that of the D/h = 0.5 case and was the same as the difference between the characteristic frequencies of the free jet vortices and the secondary vortices. According to the previous heat transfer studies for impinging jet on a circular cylinder, the averaged Nusselt number was found to increase with decreasing curvature ratio D/h. Therefore, it is possible to postulate that alternate vortex shedding is responsible for higher heat transfer and is thus a more efficient flow structure than induced symmetrical secondary vortices only.
Author:
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Category : Aeronautics
Languages : en
Pages : 704
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Author:
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ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 1090
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1264
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