Vortex Core and Its Effects on the Stability of Vortex Flow over Slender Conical Bodies

2005 ◽  
Author(s):  
Jinsheng Cai ◽  
Her-Mann Tsai ◽  
Shijun Luo ◽  
Feng Liu
Keyword(s):  
Vortex Core ◽  
Vortex Flow ◽  
The Stability

Development and Effects of Super-Critical Taylor-Vortex Flow in a Lightly Loaded Journal Bearing

1974 ◽  
Vol 96 (1) ◽  
pp. 28-35 ◽  
Author(s):  
R. C. DiPrima ◽  
J. T. Stuart
Keyword(s):  
Vortex Flow ◽  
Axial Direction ◽  
Basic Flow ◽  
Circular Cylinders ◽  
Taylor Vortex ◽  
Taylor Vortices ◽  
Taylor Vortex Flow ◽  
Secondary Motion ◽  
The Stability ◽  
Unified Description

At sufficiently high operating speeds in lightly loaded journal bearings the basic laminar flow will be unstable. The instability leads to a new steady secondary motion of ring vortices around the cylinders with a regular periodicity in the axial direction and a strength that depends on the azimuthial position (Taylor vortices). Very recently published work on the basic flow and the stability of the basic flow between eccentric circular cylinders with the inner cylinder rotating is summarized so as to provide a unified description. A procedure for calculating the Taylor-vortex flow is developed, a comparison with observed properties of the flow field is made, and formulas for the load and torque are given.

scholarly journals Slit Wall Effect on the Stability of Wavy Vortex Flow

2014 ◽  
Vol 6 ◽  
pp. 853069 ◽  
Author(s):  
Dong Liu ◽  
Ying-ze Wang ◽  
Hyoung-Bum Kim ◽  
Fang-neng Zhu ◽  
Chun-lin Wang
Keyword(s):  
Numerical Simulation ◽  
Flow Field ◽  
Radial Velocity ◽  
Flow Regime ◽  
Experimental Measurement ◽  
Vortex Flow ◽  
Wall Effect ◽  
Taylor Vortices ◽  
Simulation Results ◽  
The Stability

The wavy vortex flow in the plain model was studied by experimental measurement; the preliminary feature of wavy vortex flow was obtained. This flow field in the plain model was also studied by numerical simulation. The reliability of numerical simulation was verified by comparing with the experimental and numerical simulation results. To study the slit wall effect on the wavy vortex flow regime, another two models with different slit number were considered; the slit number was 6 and 12. By comparing the wavy vortex flow field in different models, the axial fluctuation of Taylor vortices was found to be different, which was increased with the increasing of slit number. The maximum radial velocity from the inner cylinder to the outer one in the 6-slit number was increased by 12.7% compared to that of plain model. From the results of different circumferential position in the same slit model, it can be found that the maximum radial velocity in slit plane is significantly greater than that in other planes. The size of Taylor vortices in different models was also calculated, which was found to be increased in the 6-slit model but was not changed as the slit number increased further.

Numerical Experiments for Flow Around a Ducted Tip Hydrofoil

2002 ◽  
Author(s):  
Hildur Ingvarsdo´ttir ◽  
Carl Ollivier-Gooch ◽  
Sheldon I. Green
Keyword(s):  
Turbulence Model ◽  
Vortex Core ◽  
Vortex Flow ◽  
Computational Study ◽  
Near Field ◽  
Vortex Formation ◽  
Tip Vortex ◽  
Navier Stokes ◽  
Computational Studies ◽  
Tip Vortices

The performance and cavitation characteristics of marine propellers and hydrofoils are strongly affected by tip vortex behavior. A number of previous computational studies have been done on tip vortices, both in aerodynamic and marine applications. The focus, however, has primarily been on validating methods for prediction and advancing the understanding of tip-vortex formation in general, rather than showing effects of tip modifications on tip vortices. Studies of the most relevance to the current work include computational studies by Dacles-Mariani et al. (1995) and Hsiao and Pauley (1998, 1999). Daeles-Mariani et al. carried out interactively a computational and experimental study of the wingtip vortex in the near field using a full Navier-Stokes simulation, accompanied with the Baldwin-Barth turbulence model. Although they showed improvement over numerical results obtained by previous researchers, the tip vortex strength was underpredicted. Hsiao and Pauley (1998) studied the steady-state tip vortex flow over a finite-span hydrofoil, also using the Baldwin-Barth turbulence model. They were able to achieve good agreement in pressure distribution and oil flow pattern with experimental data and accurately predict vertical and axial velocities of the tip vortex core within the near-field region. Far downstream, however, the computed flow field was overly diffused within the tip vortex core. Hsiao and Pauley (1999) also carried out a computational study of the tip vortex flow generated by a marine propeller. The general characteristics of the flow were well predicted but the vortex core was again overly diffused.

The effect of radius ratio on the stability of Couette flow and Taylor vortex flow

1984 ◽  
Vol 27 (10) ◽  
pp. 2403 ◽  
Author(s):  
R. C. DiPrima ◽  
P. M. Eagles ◽  
B. S. Ng
Keyword(s):  
Couette Flow ◽  
Vortex Flow ◽  
Radius Ratio ◽  
Taylor Vortex ◽  
Taylor Vortex Flow ◽  
The Stability

An Experimental Investigation of the Stability of Spiral Vortex Flow

1979 ◽  
Vol 21 (6) ◽  
pp. 397-402 ◽  
Author(s):  
M. M. Sorour ◽  
J. E. R. Coney
Keyword(s):  
Vortex Flow ◽  
Outer Cylinder ◽  
Axial Flow ◽  
Reynolds Numbers ◽  
Taylor Vortex ◽  
Vortex Cell ◽  
Annular Gap ◽  
Spiral Vortex ◽  
Axial Pressure Gradient ◽  
The Stability

The hydrodynamic stability of the flow in an annular gap, formed by a stationary outer cylinder and a rotatable inner cylinder, through which an axial flow of air can be imposed, is studied experimentally. Two annulus radius ratios of 0.8 and 0.955 are considered, representing wide- and narrow-gap conditions, respectively. It is shown that, when a large, axial pressure gradient is superimposed on the tangential flow induced by the rotation of the inner cylinder, the characteristics of the flow at criticality change significantly from those at zero and low axial flows, the axial length and width of the resultant spiral vortex departing greatly from the known dimensions of a Taylor vortex cell at zero axial flow. Also, the drift velocity of the spiral vortex is found to vary with the axial flow. Axial Reynolds numbers, Rea, of up to 700 are considered.

Prediction of Propeller Tip Vortex Using OpenFOAM

2017 ◽  
Author(s):  
Md Ashim Ali ◽  
Heather Peng ◽  
Wei Qiu ◽  
Rickard Bensow
Keyword(s):  
Vortex Core ◽  
Eddy Viscosity ◽  
Vortex Flow ◽  
Unstructured Grid ◽  
Turbulence Models ◽  
Tip Vortex ◽  
Navier Stokes ◽  
Taylor Model ◽  
Navier Stokes Equation ◽  
Thrust And Torque

It is important to predict the propeller tip vortex flow and its effect on hull vibration and noise. In our previous work, the tip vortex flow of the David Taylor Model Basin (DTMB) 5168 propeller model has been studied based on the Reynolds Averaged Navier-Stokes equation (RANS) solution using various eddy viscosity and Reynolds Stress turbulence models. A set of structural grids were used, however, large Jacobian values of the structural grids around the propeller tip region led to the convergence problem and inaccurate solutions. In the present work, the numerical prediction of the same propeller model was improved by using a steady-state RANS solver simpleFoam in OpenFOAM with locally refined unstructured grid along the tip vortex trajectory. The computed thrust and torque coefficients and the velocity components across the vortex core are compared with experimental data and results in the previous studies. Improvement in the prediction of velocity components across the tip vortex core were achieved.

The behaviour of vortex lines near a wire in liquid helium II

1964 ◽  
Vol 277 (1369) ◽  
pp. 214-236 ◽  
Keyword(s):  
Vortex Core ◽  
Vortex Line ◽  
Core Radius ◽  
Potential Barriers ◽  
Helium Ii ◽  
Upper Limit ◽  
Vortex Lines ◽  
Large Vortex ◽  
The Wire ◽  
The Stability

By the application of classical hydrodynamics to the interaction between a wire and a parallel vortex line it is shown that states having different numbers of quanta of superfluid circulation about the wire are separated by high potential barriers. Possible ways of overcoming or avoiding the barriers are discussed, and it is concluded that such states are normally metastable. A method for finding steady vortex-line configurations is then developed, and it is found that, in an apparatus of the type used by Vinen (1961 b ) to detect single quanta of circulation, states having vortex lines partly attached to the wire are metastable in certain circumstances. These results are compared with Vinen’s account of his experiment. They agree well with the observations made when the apparatus had ceased to rotate. During rotation some points remain puzzling, but the failure to attain equilibrium, ascribed by Vinen to an anomalously large vortex core, is now seen to arise from the trapping of vortex lines in metastable states. A critical superfluid velocity of about 10 3 cm/s for the creation of vortex lines at a solid surface is derived, and, from this and the experimental observation of the stability of integral circulation about the wire against vibration, an upper limit of 3 x 10 -6 cm to the vortex core radius is tentatively deduced. It is concluded that the theory of quantized vortex lines of small (≈ 10 -7 cm) core radius can account fairly well for the observations. Further possible tests of the theory are suggested.

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