scholarly journals Laminar and turbulent comparisons for channel flow and flow control

2007 ◽  
Vol 570 ◽  
pp. 467-477 ◽  
Author(s):  
IVAN MARUSIC ◽  
D. D. JOSEPH ◽  
KRISHNAN MAHESH
Keyword(s):  
Pressure Gradient ◽  
Flow Control ◽  
Turbulent Flows ◽  
Control Strategies ◽  
Reynolds Numbers ◽  
Volume Flux ◽  
Reynolds Number Flow ◽  
Number Flow ◽  
High Reynolds ◽  
Strategy Design

A formula is derived that shows exactly how much the discrepancy between the volume flux in laminar and in turbulent flow at the same pressure gradient increases as the pressure gradient is increased. We compare laminar and turbulent flows in channels with and without flow control. For the related problem of a fixed bulk-Reynolds-number flow, we seek the theoretical lowest bound for skin-friction drag for control schemes that use surface blowing and suction with zero-net volume-flux addition. For one such case, using a crossflow approach, we show that sustained drag below that of the laminar-Poiseuille-flow case is not possible. For more general control strategies we derive a criterion for achieving sublaminar drag and use this to consider the implications for control strategy design and the limitations at high Reynolds numbers.

Coherent structures in coflowing jets and wakes

1978 ◽  
Vol 88 (3) ◽  
pp. 451-463 ◽  
Author(s):  
A. E. Perry ◽  
T. T. Lim
Keyword(s):  
Large Scale ◽  
Three Dimensional ◽  
Glass Tube ◽  
Reynolds Numbers ◽  
Reynolds Number Flow ◽  
Naturally Occurring ◽  
Number Flow ◽  
High Reynolds ◽  
Scale Motion

By applying small lateral oscillations to a glass tube from which smoke was issuing, perfectly periodic coflowing jets and wake structures were produced at Reynolds numbers of order 300-1000. These structures remained coherent over long streamwise distances and appeared to be perfectly frozen when viewed under stroboscopic light which was synchronized with the disturbing oscillation. By the use of strobing laser beams, longitudinal sections of the structures were photographed and an account of the geometry of these structures is reported.When the tube was unforced, similar structures occurred but they modulated in scale and frequency, and their orientation was random.A classification of structures is presented and examples are demonstrated in naturally occurring situations such as smoke from a cigarette, the wake behind a three-dimensional blunt body, and the high Reynolds number flow in a plume from a chimney. It is suggested that an examination of these structures may give some insight into the large-scale motion in fully turbulent flow.

Development of localized arc filament RF plasma actuators for high-speed and high Reynolds number flow control

2010 ◽  
Vol 49 (2) ◽  
pp. 497-511 ◽  
Author(s):  
J.-H. Kim ◽  
M. Nishihara ◽  
I. V. Adamovich ◽  
M. Samimy ◽  
S. V. Gorbatov ◽  
...  
Keyword(s):  
Reynolds Number ◽  
Flow Control ◽  
High Speed ◽  
High Reynolds Number ◽  
Plasma Actuators ◽  
Rf Plasma ◽  
Reynolds Number Flow ◽  
Number Flow ◽  
High Reynolds

Study on Spacer Grid Span Pressure Loss Under High Reynolds Number Flow Condition

2009 ◽  
Author(s):  
Kazuo Ikeda ◽  
Yasunao Yamaguchi ◽  
Juntaro Shimizu ◽  
Kaoru Okamoto
Keyword(s):  
Reynolds Number ◽  
Flow Condition ◽  
Pressure Loss ◽  
Reynolds Numbers ◽  
Cfd Model ◽  
Spacer Grid ◽  
Reynolds Number Flow ◽  
Rod Bundle ◽  
Number Flow ◽  
High Reynolds

Pressure loss coefficient of spacer grid is used as a key parameter for PWR core thermal hydraulic design. It has been obtained by single-phase hydraulic testing for many years. However, it is necessary to develop design tool for precise estimation of pressure loss of spacer grids as well as hydraulic tests to meet the needs of the worldwide nuclear fuel market. Recently, Computational Fluid Dynamics (CFD) analysis has been applied for estimation of flow field in a fuel rod bundle. In this study, the numerical simulation in a range of bare rod Reynolds numbers of the reactor flow condition is performed to examine the applicability of the CFD model for estimating spacer grid span pressure loss. For verification of the numerical estimation, the span pressure loss of 5×5 rod bundle with spacer grid is measured in Nuclear Development Corporation (NDC) hydraulic test facility up to bare rod Reynolds number as high as 500,000. The simulation shows good agreement with experimental data in the range of Reynolds numbers. The CFD model is also utilized to investigate the pressure loss as a function of distance from last passed spacer grid and to discuss the turbulent flow characteristics in the rod bundle with spacer grid under high Reynolds number flow condition.

High Reynolds number flow between torsionally oscillating disks

1970 ◽  
Vol 2 (1) ◽  
pp. 55-79
Author(s):  
K.G. Smith ◽  
A.F. Pillow
Keyword(s):  
Boundary Layers ◽  
Viscous Incompressible Fluid ◽  
Reynolds Numbers ◽  
Main Body ◽  
Low Reynolds Numbers ◽  
Reynolds Number Flow ◽  
High Reynolds Numbers ◽  
Number Flow ◽  
High Reynolds ◽  
Steady Convection

In this paper the problem solved is that of unsteady flow of a viscous incompressible fluid between two parallel infinite disks, which are performing torsional oscillations about a common axis. The solution is restricted to high Reynolds numbers, and thus extends an earlier solution by Rosenblat for low Reynolds numbers.The solution is obtained by the method of matched asymptotic expansions. In the main body of the fluid the flow is inviscid, but may be rotational, and in the boundary layers adjacent to the disks the non-linear convection terms are small. These two regions do not overlap, and it is found that in order to match the solutions a third region is required in which viscous diffusion is balanced by steady convection. The angular velocity is found to be non-zero only in the boundary layers adjacent to the disks.

Pressure and Vortex Shedding Patterns Around a Low Aspect Ratio Cylinder in a Sheared Flow at Transitional Reynolds Numbers

1981 ◽  
Vol 103 (1) ◽  
pp. 88-95 ◽  
Author(s):  
D. M. Rooney ◽  
R. D. Peltzer
Keyword(s):  
Reynolds Number ◽  
Vortex Shedding ◽  
Reynolds Numbers ◽  
Pressure Measurements ◽  
Reynolds Number Flow ◽  
Sheared Flow ◽  
Number Flow ◽  
High Reynolds ◽  
First Time ◽  
Upstream Flow

Model tests were performed in a wind tunnel to determine vortex shedding patterns induced around a circular cylinder by spanwise shear in transitional Reynolds number flow. In addition, mean and fluctuating pressure measurements were obtained. The introduction of shear in the upstream flow generated two distinct cells of vortex frequencies behind the cylinder in the transcritical regime, thereby documenting for the first time that the re-established high Reynolds number shedding closely parallels patterns already observed in subcritical flow. The two cell pattern did not permit any correlation between shear level and cell length to be found.

Low Reynolds Number Flow Computations of a Sphere With Slip

2005 ◽  
Author(s):  
O. Pulat ◽  
R. N. Parthasarathy
Keyword(s):  
Reynolds Number ◽  
Drag Coefficient ◽  
Reynolds Numbers ◽  
Water Medium ◽  
Reynolds Number Flow ◽  
Drag Forces ◽  
Falling Sphere ◽  
Number Flow ◽  
High Reynolds ◽  
Flow Past A Sphere

A computational fluid dynamics package (FLUENT) was used to simulate the conditions of a falling sphere through a water medium with a zero shear stress condition (full slip) for Reynolds numbers in the range. Comparisons of the results were made with simulations of the flow past a sphere with no slip. Specific differences were observed in the drag coefficient, drag forces, axial velocity, radial velocity, and wake characteristics. A significant reduction in the drag coefficient was observed with the presence of slip on the surface. With a decrease in the Reynolds number the decreases in the wake structure became negligible, however, the differences in drag coefficient became significant. At high Reynolds numbers, the wake was skewed towards the rear of the sphere, under the full slip condition.

On the low-Reynolds-number flow in a helical pipe

1981 ◽  
Vol 108 ◽  
pp. 185-194 ◽  
Author(s):  
C. Y. Wang
Keyword(s):  
Reynolds Number ◽  
Flow Rate ◽  
Reynolds Numbers ◽  
Order Unity ◽  
Low Reynolds Number Flow ◽  
Reynolds Number Flow ◽  
Helical Pipe ◽  
Number Flow ◽  
High Reynolds ◽  
Curvature And Torsion

A non-orthogonal helical co-ordinate system is introduced to study the effect of curvature and torsion on the flow in a helical pipe. It is found that both curvature and torsion induce non-negligible effects when the Reynolds number is less than about 40. When the Reynolds number is of order unity, torsion induces a secondary flow consisting of one single recirculating cell while curvature causes an increased flow rate. These effects are quite different from the two recirculating cells and decreased flow rate at high Reynolds numbers.

High Reynolds Number Flow Tests of Flexible Cylinders With Helical Strakes

2006 ◽  
Author(s):  
Don W. Allen ◽  
Dean L. Henning ◽  
Li Lee
Keyword(s):  
Reynolds Numbers ◽  
Circular Cylinders ◽  
Test Results ◽  
Reynolds Number Flow ◽  
Helical Strakes ◽  
Number Flow ◽  
Pvc Pipe ◽  
High Reynolds ◽  
Naval Surface Warfare ◽  
Cylinder Drag

Tow tests have been performed on flexible circular cylinders, with and without short helical strakes, towed in a basin at critical and supercritical Reynolds numbers. The tests were conducted at the Naval Surface Warfare Center’s David Taylor Model Basin in Carderock, Maryland. Measurements were made of both the drag and acceleration (due to vortex-induced vibration) of the cylinder. A 3-1/2 inch diameter ABS pipe was used to achieve Reynolds numbers ranging from about 2×105 to 5×105, and a 5-9/16-inch diameter PVC pipe was used to achieve Reynolds numbers ranging from about 7×105 to 1.5×106. Tests were also conducted with aluminum inserts (strong-backs), made to fit just inside the test cylinders, in order to obtain stationary (rigid) cylinder drag measurements for comparison purposes. The test results for cylinders fitted with triple-start helical strakes are presented in this paper.

High Reynolds number flow past a flat 'plate with strong blowing

1972 ◽  
Vol 51 (2) ◽  
pp. 337-356 ◽  
Author(s):  
J. B. Klemp ◽  
A. Acrivos
Keyword(s):  
Boundary Layer ◽  
Flat Plate ◽  
Free Stream ◽  
Reynolds Numbers ◽  
Reynolds Number Flow ◽  
Flow Past ◽  
Number Flow ◽  
Flow Domain ◽  
High Reynolds ◽  
Matching Techniques

For the uniform flow past a semi-infinite flat plate subject to a blowing velocity profile equal to C(Uv/x),½ the conventional boundary-layer approximations break down as C approaches 0middot;6192. Here, we consider the structure of the flow for large Reynolds numbers R when C exceeds this critical value. It is shown that, for C > 0·6192, a region containing injected fluid O(R-1/3)) in thickness forms directly above the plate. To a first approximation the flow in this region is inviscid and the pressure a function of x only. This blowing region is separated from the free stream by a free shear boundary layer of thickness O(R-½). Thus the flow domain consists of three distinct regions which interact to yield a similarity solution valid for large values of Rx. This solution is then extended to higher order by expanding the stream function in each region in powers of (Rx)-1/3 and evaluating the first four terms in the resulting series using standard matching techniques. Finally, more general blowing profiles which also lead to boundary-layer ‘blow off’ are considered and an expression, valid far downstream of boundary-layer detachment, is derived for the position of the streamline separating the injected fluid from that of the free stream. For the case of uniform blowing the blowing region takes on the shape of a wedge, indicating that no solution can exist for the corresponding external flow if the plate is truly semi-infinite.

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