INFLUENCE OF COHERENT STRUCTURES ON THE WALL SHEAR STRESS IN AXIAL FLOW BETWEEN A CYLINDER AND A PLANE WALL

Author(s):  
Imed Khabbouchi ◽  
Mohamed Sadok Guellouz ◽  
Stavros Tavoularis
2009 ◽  
Vol 633 ◽  
pp. 147-158 ◽  
Author(s):  
SEBASTIAN GROSSE ◽  
WOLFGANG SCHRÖDER

The wall-shear stress distribution in turbulent duct flow has been assessed using the micro-pillar shear-stress sensor MPS3. The spatial resolution of the sensor line is 10.8l+(viscous units) and the total field of view of 120l+along the spanwise direction allows to capture characteristic dimensions of the wall-shear stress distribution at sufficiently high resolution. The results show the coexistence of low-shear and high-shear regions representing ‘footprints’ of near-wall coherent structures. The regions of low shear resemble long meandering bands locally interrupted by areas of higher shear stress. Conditional averages of the flow field indicate the existence of nearly streamwise counter-rotating vortices aligned in the streamwise direction. The results further show periods of very strong spanwise wall-shear stress to be related to the occurrence of high streamwise shear regions and momentum transfer towards the wall. These events go along with a spanwise oscillation and a meandering of the low-shear regions.


2010 ◽  
Vol 651 ◽  
pp. 165-209 ◽  
Author(s):  
R. RANJAN ◽  
C. PANTANO ◽  
P. FISCHER

Turbulent swept flow over a cylindrical wire placed on a wall of a channel is investigated using direct numerical simulations. This geometry is a model of the flow through the wire-wrapped fuel pins, the heat exchanger, typical of many nuclear reactor designs. Mean flow along and across the wire axis is imposed, leading to the formation of separated flow regions. The Reynolds number based on the bulk velocity along the wire axis direction and the channel half height is 5400 and four cases are simulated with different flowrates across the wire. This configuration is topologically similar to backward-facing steps or slots with swept flow, except that the dominant flow is along the obstacle axis in the present study and the crossflow is smaller than the axial flow, i.e. the sweep angle is large. Mean velocities, turbulence statistics, wall shear stress and instantaneous flow structures are investigated. Particular attention is devoted to the statistics of the shear stress on the walls of the channel and the wire in the recirculation zone. The flow around the mean reattachment region, at the termination of the recirculating bubble, does not exhibit the typical decay of the mean shear stress observed in classical backward-facing step flows owing to the presence of a strong axial flow. The evolution of the mean wall shear stress angle after reattachment indicates that the flow recovers towards equilibrium at a rather slow rate, which decreases with sweep angle. Finally, the database is analysed to estimate resolution requirements, in particular around the recirculation zones, for large-eddy simulations. This has implications in more complete geometrical models of a wire-wrapped assembly, involving hundreds of fuel pins, where only turbulence modelling can be afforded computationally.


1986 ◽  
Vol 108 (2) ◽  
pp. 166-172 ◽  
Author(s):  
M. Abdelghany ◽  
R. Eichhorn

Hot film probe measurements of the distribution of the wall shear stress were made for axial flow along a rectangular 3 × 6 array of rods with a pitch to diameter ratio, P/D = 4/3, and a wall to diameter ratio, W/D = 2/3. Measurements were performed on rods at several locations and on two duct side walls at a position 62 hydraulic diameters from the entrance. Local shear stress maxima occur near the largest subchannel flow areas with the lowest maximum local shear stress on rods nearest the sidewalls. Maximum to the minimum shear stress ratio on an individual rod is largest for the corner rod. Side wall maximum local shear stress occurs in the first wall subchannel. Overall friction factors calculated from the wall shear stress measurements agree with those calculated from pressure drop data.


1969 ◽  
Vol 91 (4) ◽  
pp. 728-733 ◽  
Author(s):  
R. G. Backshall ◽  
Fred Landis

An experimental study was performed to determine the boundary-layer characteristics of an incompressible swirl flow produced by the insertion of a helically twisted tape into a pipe. The resulting flow can be approximated by a uniform axial flow with a superposed forced vortex flow. Boundary-layer velocity measurements indicate that the total velocity in this three-dimensional flow is well approximated by the universal logarithmic velocity profile. Modified axial and tangential logarithmic velocity laws have also been derived and are shown to be in good agreement with the data. The wall shear stress has to be determined either by direct velocity gradient measurements at the wall or by a modified momentum balance since pressure loss measurements do not directly lead to the correct wall shear stress.


Author(s):  
Sangjin Ryu ◽  
Ethan Davis ◽  
Jae Sung Park ◽  
Haipeng Zhang ◽  
Jung Yoo

Abstract Coherent structures are critical for controlling turbulent boundary layers due to their roles in momentum and heat transfer in the flow. Turbulent coherent structures can be detected by measuring wall shear stresses that are footprints of coherent structures. In this study, wall shear stress fluctuations were measured simultaneously in a zero pressure gradient turbulent boundary layer using two house-made wall shear stress probes aligned in the spanwise direction. The wall shear stress probe consisted of two hot-wires on the wall aligned in a V-shaped configuration for measuring streamwise and spanwise shear stresses, and their performance was validated in comparison with a direct numerical simulation result. Relationships between measured wall shear stress fluctuations and streamwise velocity fluctuations were analyzed using conditional sampling techniques. The peak detection method and the variable-interval time-averaging (VITA) method showed that quasi-streamwise vortices were inclined toward the streamwise direction. When events were simultaneously detected by the two probes, stronger fluctuations in streamwise velocity were detected, which suggests that stronger coherent structures were detected. In contrast to the former two methods, the hibernating event detection method detects events with lower wall shear stress fluctuations. The ensemble-averaged mean velocity profile of hibernating events was shifted upward compared to the law of the wall, which suggests low drag status of the coherent structures related with hibernating events. These methods suggest significant correlations between wall shear stress fluctuations and coherent structures, which could motivate flow control strategies to fully exploit these correlations.


1971 ◽  
Vol 93 (2) ◽  
pp. 102-108 ◽  
Author(s):  
L. S. Galowin ◽  
M. J. Desantis

A theoretical investigation was conducted to obtain velocity, pressure, and shear stress distributions for incompressible, steady, fully developed, laminar flow through a cylinder with a uniformly porous wall. Ejection/injection at the walls results from the pressure difference across the porous wall. Fluid flow phenomena in porous tubes and ducts have previously been investigated with the velocity prescribed as the boundary condition at the wall. An accurate wall condition must account for the variable wall velocity being dependent upon the pressure difference across the wall, the properties of the fluid, the thickness and the permeability of the structure. An integral momentum technique was employed to reduce the axisymmetric Navier-Stokes equations in cylindrical coordinates to a nonlinear, second-order ordinary differential equation with appropriate boundary conditions. The velocity condition at the wall was established for the ejection/injection at the surface resulting from the pressure difference across the porous wall derived from Darcy’s law. Numerical solutions were obtained for a range of axial flow Reynolds numbers, wall permeabilities, and initial pressure difference across the porous wall. The calculated static pressure variation in the axial flow direction, the velocity components, and the wall shear stress are presented. For the case of fluid ejection, the results of the analysis show that the wall shear stress and static pressure decrease in the axial flow direction. The rates of decrease are functions of the wall porosity, initial pressure gradient across the wall, and inlet flow Reynolds number. The present analysis treats the realistic problem of flow adjustment to the condition where zero pressure differential across the porous wall occurs (the normal wall velocity vanishes). Previous models are based upon the assumptions of constant radial velocity at the wall and/or prescribed wall shear stress without taking into account the pressure drop through the wall. Such assumptions imply that a variable pressure exists external to the pipe, or that the pipe has walls of variable permeability and thickness rather than the hypothesized condition that the pipe has uniformly porous walls. For one set of boundary conditions it is shown that the outflow through the walls completely discharges the entering flow. As a result no far downstream axial flow occurs. Such effects were not previously discussed by other investigators. For other sets of boundary conditions reductions in centerline velocity and shear stress occur.


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