tutorial 8. non-newtonian transitional flow in an...

Tutorial 8. Non-Newtonian Transitional Flow in anEccentric Annulus

Introduction

The purpose of this tutorial is to illustrate the setup and solution of a 3D, turbulent flowof a non-Newtonian fluid.

Turbulent non-Newtonian flows are often encountered in the oil and gas industry. Thesefluids are used in the drilling of oil wells to transport the cuttings to the surface, andto keep solids in suspension during stationary periods. In directional drilling, where aneccentric annulus is often used, there is a tendency for the cuttings to accumulate inthe narrowest gap where the velocity is lowest. Since turbulence tends to suppress suchaccumulation, knowledge of the velocity profiles in the annulus are essential in the designand operation of these drills.

In this tutorial, you will learn how to:

• Read an existing mesh file in FLUENT.

• Check the grid for dimensions and quality.

• Set up the material for non-Newtonian viscosity and switch to turbulence formula-tion for the same using text user interface (TUI) commands.

• Solve a time dependent simulation.

• Set up periodic flow conditions in FLUENT.

• Set up transitional flow conditions using k − ω turbulence model.

• Create isosurfaces and isoclips for postprocessing.

• Examine the results and compare them with experimental data.

Prerequisites

This tutorial assumes that you have little experience with FLUENT but are familiar withthe interface.

c© Fluent Inc. August 18, 2005 8-1

Non-Newtonian Transitional Flow in an Eccentric Annulus

Problem Description

A periodic section of the eccentric annulus arrangement is considered (Figure 8.1). Theinner and outer cylinders diameters are 20 mm and 40.3 mm respectively. The innercylinder is rotating with speed of 300 rpm whereas the outer one is stationary. Theviscosity is governed by the Power law as:

µ = K × γ(n−1)

where,

n = power law index = 0.75K = consistency index = 0.044γ = local shear rate

The flow is considered to be in transitional regime with Re = 9000.

Figure 8.1: Problem Schematic

8-2 c© Fluent Inc. August 18, 2005


Preparation

1. Copy the following files to your working directory:

• annulus.msh

• non-dimensional.scm

• axial-p1.xy

• axial-p2.xy

• axial-p3.xy

• tangential-p1.xy



2. Start the 3D double precision solver of FLUENT.

Setup and Solution

Step 1: Grid

1. Read the mesh file, annulus.msh.

File −→ Read −→Case...

FLUENT will read the mesh file and report the progress in the console window.

2. Check the grid.

Grid −→Check

This procedure checks the integrity of the mesh. Make sure the reported minimumvolume is a positive number.

3. Check the scale of the grid.

Grid −→Scale...

Check the domain extents to see if they correspond to the actual physical dimensions.If not, the grid has to be scaled with proper units. In this case, the outer diametershould be 40.3 mm, therefore scale the grid in mm.



(a) Select mm in the Grid Was Created In drop-down list.

(b) Click Scale and close the panel.

4. Display the grid (Figures 8.2).

Display −→Grid...

The color for each periodic boundary is Cyan and for each wall it is White. FLUENTwill automatically color each boundary based on its type.



5. Remove the Hidden lines.

Display −→Options...

(a) Enable Hidden Line Removal and click Apply.

Figure 8.2: Grid Display

To capture the sharp gradients near the walls correctly, the grid adjacent to thewalls is made finer compared to the central region. In addition, as the problem isturbulent it is essential to meet the correct Y+ conditions as per the wall treatmentto be used.



Step 2: Models

The flow has Reynolds number of 9000, and it needs to be modeled as turbulent. Thek − ω model can be used for such low Reynolds number, turbulent, or transitional flows.

Re =ρ× Ub × dh

µ(8.1)

In this case, the mass flow rate = 2.615 kg/s. Therefore, the bulk velocity can becalculated as: Bulkvelocity = Massflow

Density×Area= 2.615

1000×0.00961

Where,

ρ = density of the fluid = 1000 kg/m3Ub = bulk velocity = 2.72 m/sdh = hydraulic diameter (Do-Din) = 20.3× 10−3

µ = viscosity at the wall = 6× 10−3 (measured experimentally [1])

1. Enable viscous model.

Define −→ Models −→Viscous...

(a) Under Model, select k-omega (2 eqn).

(b) Under k-omega Options, enable Transitional Flows.

(c) Click OK.



Step 3: Materials

1. Change the material properties.

Define −→Materials...

(a) There is no model that can be used for viscosity as we need non-Newtonianpower law. To enable the model, issue the text user interface command as:

define/models/viscous/turbulence-expert/turb-non-newtonian

Enable turbulence for non-Newtonian fluids? [no] yes



(b) In the materials panel, select non-newtonian-power-law in the Viscosity drop-down list.

This opens Non-Newtonian Power Law panel.

i. Specify the following parameters:

Parameter ValueConsistency Index 0.044

Power-Law Index 0.75

Reference Temperature 0

Minimum Viscosity Limit 0.0001

Maximum Viscosity Limit 1000

ii. Click OK.

(c) Set Density to 1000.

(d) Specify Name as cmc and click Change/Create.

(e) Click NO when FLUENT asks Change/Create mixture and overwrite air?

(f) Close the materials panel.

FLUENT automatically enables the energy equation as non-Newtonian powerlaw formulation is being used. You can disable it from the solution afterwards.



Step 4: Units

1. Change the units for angular-velocity to rpm.

Define −→Units...

(a) Under Quantities, select angular-velocity.

(b) Under Units, select rpm and close the panel.

Step 5: Boundary Conditions

1. Set the boundary conditions for fluid.

Define −→Boundary Conditions...

(a) Under Zone, select fluid.

The Type will be reported as fluid.

(b) Click Set....

The Fluid panel opens.



i. Select cmc in the Material Name drop-down list.

ii. Click OK to accept the settings and close the panel.

2. Set the boundary conditions for inner.

(a) Under Zone, select inner.

The Type will be reported as wall.

(b) Click Set....

The Wall panel opens.



i. Select Momentum tab.

ii. Under Wall Motion, enable Moving Wall.

iii. Under Motion, enable Rotational and specify a value of 300 for Speed.

iv. Click OK.

Step 6: Periodic Conditions

1. Specify the flow rate across periodic boundaries.

Define −→Periodic Conditions...



(a) Under Type, enable Specify Mass Flow.

(b) Under Flow Direction, set the values of X, Y, and Z to 0, 0, and 1 respectively.

(c) Specify a value of 2.615 for Mass Flow Rate.

(d) Click OK to accept the settings and close the panel.

Step 7: Solution

1. Set the solution controls.

Solve −→ Controls −→Solution...

(a) Under Equations, deselect Energy.

The viscosity is function of shear stress (does not depend on the temperature).Therefore, there is no need to solve the energy equation.

(b) Retain other settings and click OK.

2. Initialize the flow.

Solve −→ Initialize −→Initialize...



(a) Set Z Velocity (m/s) to 2.72.

From Equation 8.1, bulk velocity was calculated as 2.72.

(b) Set Turbulence Kinetic Energy to 0.01.

(c) Set Specific Dissipation Rate to 0.01.

(d) Click Init and close the panel.

3. Enable plotting of residuals during the calculation.

Solve −→ Monitors −→Residuals...

(a) Under Options, enable Plot.

(b) Click OK.

4. Save the case file (annulus1.cas.gz).

File −→ Write −→Case...



Retain the default activated Write Binary Files option so that you can write a binaryfile. The .gz option will save zipped files, this will work on both, Windows as wellas UNIX platforms.

5. Iterate the solution.

Solve −→Iterate...

(a) Set Number of Iterations to 400.

(b) Click Iterate to start the calculation.

The solution converges in 283 iterations. The residuals plot is shown in Fig-ure 8.3.



Figure 8.3: Scaled Residuals

6. Switch to higher order upwind schemes.

Solve −→ Controls −→Solution...

(a) Under Discretization, select QUICK for Momentum, Turbulence Kinetic Energy,and Specific Dissipation Rate.

(b) Click OK.

Convergence can be detected by monitoring some key parameter during theiterations. In this case you will monitor turbulence kinetic energy over centralplane of the domain. To do so, create an isosurface at the correspondinglocation in the domain.



7. Create an isosurface.

Surface −→Iso-Surface...

(a) Under Surface of Constant, select Grid... and Y-Coordinate.

(b) Under Iso-Values, enter 0.

(c) Under New Surface Name, enter y=0.

(d) Click Create and close the panel.

8. Monitor the turbulence kinetic energy over the isosurface.

Solve −→ Monitor −→Surface...

(a) Increase Surface Monitors to 1.

(b) Enable Plot and Print for monitor-1.

(c) Click Define...

This opens Define Surface Monitor panel.



i. Select Area Weighted Average in the Report Type drop-down list.

ii. Select Turbulence... and Turbulence Kinetic Energy in the Reports of drop-down lists.

iii. Under Surface, select y=0.

iv. Click OK.

(d) Click OK in the Surface Monitors panel.

The average value of turbulence kinetic energy on y=0 plane will be plotted inthe graphics window and printed on the console during the iterations.

9. Disable convergence criteria for all equations.

Solve −→ Monitors −→Residuals...

(a) Disable Check Convergence for all equations.

(b) Click OK.



10. Iterate the solution till the convergence is achieved.

Solve −→Iterate...

(a) Set Number of Iterations to 5000.

(b) Click Iterate to start the calculation.

The solution will converge in around 4500 iterations. It is observed that themonitor plot is almost flat and you can stop the computation.

Figure 8.4: Convergence History of Turbulence Kinetic Energy on y=0

Figure 8.5: Scaled Residuals

11. Save the case and data files (annulus2.cas.gz and annulus2.dat.gz).

File −→ Write −→Case & Data...



Step 8: Postprocessing

1. Create an isosurface.

The flow is translationally periodic along Z direction. Create an isosurface along Zdirection to view the results.

Surface −→Iso-surface...

(a) Select Grid... and Z-Coordinate in the Surface of Constant drop-down lists.

(b) Click Compute.

Min and Max values will get updated as per the domain extents.

(c) Under Iso-Values, enter 0.005.

(d) Enter New Surface Name as z=0.005.

(e) Click Create and close the panel.

2. Display velocity vectors (Figure 8.6).

Display −→Vectors...



(a) Select Velocity, in the Vectors of drop-down list.

(b) Select Velocity... and Velocity Magnitude in the Color by drop-down lists.

(c) Under Surfaces, select z=0.005.

(d) Click Display and close the panel.

Figure 8.6: Velocity Vectors on z=0.005

3. Display filled contours of molecular viscosity (Figure 8.7).

Display −→Contours...



(a) Select Properties... and Molecular Viscosity in the Contours of drop-down lists.

(b) Under Options, enable Filled.

(c) Under Surfaces, select z=0.005.

(d) Click Display and close the panel.

Observe the shear thinning behavior of the fluid. The viscosity is less nearwalls (high shear regions) and it is high in the central part (low shear regions).

Figure 8.7: Contours of Molecular Viscosity on z=0.005



4. Calculate the pressure drop.

Define −→Periodic Conditions...

It is important to know the pressure drop in any flow system. FLUENT updatesthe pressure gradient value after every iteration in the Periodic Conditions panel.Multiply the value reported of pressure gradient by the length of periodic section toget the pressure drop value.

In literature, the results are available at three lines P1, P2 and P3 as shown inFigure 8.1. We can create them on the z= 0.005 surface.

5. Create another isosurface to view the results.

Surface −→Iso-surface...

(a) Under From Surface, select z=0.005.

(b) Select Grid... and Y-Coordinate, in the Surface of Constant drop-down lists.

(c) Under Iso-Values, retain the value of 0.

(d) Enter New Surface Name as plane.




6. Create isoclips.

Surface −→Iso-Clip...

(a) Under Clip Surface list, select plane.

(b) Select Grid... and X-Coordinate in the Clip to Values drop-down lists.

(c) Click Compute.

This will display Min and Max values of x-coordinate along plane.

(d) Specify 0 for Min.

(e) Change New Surface Name to p-1 and click Clip.

A new surface (p-1) will be added to the list of surfaces.

(f) Click Compute.

(g) Similarly, clip plane surface with a value of 0 for Max field of X-coordinate andname it as p-3.

7. Create a line.

Surface −→Line/Rake...



(a) Retain the default values of x0 and x1.

The x0 and x1 values correspond to the X center of the domain

(b) Specify a value of 0 for y0 and any number greater than 0.02015 (say 0.1, inthis case) for y1.

(c) Set z0 and z1 to 0.005.

This will place the line in the central plane.

(d) Enter p-2 as New Surface Name.


8. Display all three surfaces that you have created (Figure 8.8).

Display −→Grid...

(a) Under Surfaces, select p-1, p-2, p-3 and z=0.005.

(b) Under Edge Type, select Outline.

(c) Click Display to verify the correct positions of these planes.



Figure 8.8: Grid Display of New Surfaces

9. Read the scheme file.

To non-dimensionalize the plots along three planes p-1, p-2, and p-3, read in thescheme file provided with this tutorial. This file has the pre-defined custom fieldfunctions based on the correct values. Reading this file will make many custom fieldfunctions available for postprocessing.

File −→ Read −→Scheme...

(a) Select non-dimensional.scm and click OK.



10. View the definitions of custom field functions.

Define −→Custom Field Functions...

(a) View the definition of each custom field function by clicking Manage....

11. Read the xy files, provided with this tutorial, that contains the experimental data.

Plot −→XY Plot...

(a) Click Load File...

This opens a Select File dialog box.

i. Select axial-p1.xy, axial-p2.xy, axial-p3.xy, tangential-p1.xy,

tangential-p2.xy, and tangential-p3.xy and click OK.

This will make axial and tangential velocities available in normalized formfor comparison.



(b) Compare the normalized axial velocity along p1 (Figure 8.9).

i. Under Options, disable Node Values and Position on X axis.

ii. Select Custom Field Functions... and normalized-axial in the Y Axis Functiondrop-down lists.

iii. Select Custom Field Functions... and normalized-p1 in the X Axis Functiondrop-down lists.

iv. Under Surfaces, select p1.

v. Under File Data, select normalized-axial vs. normalized-p1 and click Plot.

Figure 8.9: FLUENT Results vs Experimental Data for Axial Velocity Component at p-1



(c) Compare normalized tangential velocity along p3 (Figure 8.10).

i. Under Options, disable Position on X axis.

ii. Select Custom Field Functions... and normalized-tangential in the Y AxisFunction drop-down lists.

iii. Select Custom Field Functions... and normalized-p3 in the X Axis Functiondrop-down lists.

iv. Under Surfaces, select p3.

v. Under File Data, select normalized-tangential vs normalized-p3 and clickPlot.

Figure 8.10: FLUENT Results vs Experimental Data for Tangential Velocity Componentat p-3



(d) Similarly, compare remaining results as shown in Figures 8.11 and 8.12.

Figure 8.11: FLUENT Results vs Experimental Data for Axial Velocity Component atp-2 and p3

Figure 8.12: FLUENT Results vs Experimental Data for Tangential Velocity Componentat p-1 and p2



Summary

This tutorial demonstrated a similarity between the axial and tangential velocity profilespredicted by FLUENT and the experimental data. You also studied, the performance ofk−ω model in transitional regime along with the non-Newtonian formulation of viscosity.The use of monitors for detecting convergence is highlighted.

References

1. J. M. Nouri and J. H. Whitelaw, Flow of Newtonian and non-Newtonian fluids inan eccentric annulus with rotation of inner cylinder, International Journal of Heatand Fluid Flow 18:236-246, 1997

Exercises/ Discussions

1. How will the results vary if:

(a) The direction of rotation of inner cylinder is reversed.

(b) The inner cylinder rotates with higher RPM.

(c) The outer cylinder is made to rotate in the same direction as that of inner cylinder.

(d) The flow is simulated as inviscid.

2. Will the same grid work if the mass flow across the periodic boundaries is increased 10times from the existing value? What changes would you suggest in the case set-up?

3. What other situation can be simulated using the same mesh file.

Links for Further Reading

• http://www.petrol.unsw.edu.au/SCOPEteaching.pdf

• http://www.clarkson.edu/subramanian/ch301/notes/nonnewtonian.pdf

• http://www.mdpi.org/entropy/papers/e6030304.pdf


http://www.petrol.unsw.edu.au/SCOPEteaching.pdf

http://www.clarkson.edu/subramanian/ch301/notes/nonnewtonian.pdf

http://www.mdpi.org/entropy/papers/e6030304.pdf

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