Analysis of hydrodynamic forces on non-spherical particles...

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Analysis of hydrodynamic forces on non-spherical particles (Spherocylinder) Rafik OUCHENE (LEMTA, CNRS) Anne TANIERE (LEMTA, CNRS) Mohammed KHALIJ (LEMTA, CNRS) Boris ARCEN (LRGP, CNRS) Coimbra, 6-8 March 2013. International workshop Fibre Suspension Flow ModellingFrench program ANR PLAYER

Transcript of Analysis of hydrodynamic forces on non-spherical particles...

Page 1: Analysis of hydrodynamic forces on non-spherical particles ...158.110.32.35/COST/downloads/SIG43_FP1005-COIMBRA... · in order to choose or develop a model that will later be introduced

Analysis of hydrodynamic forces on non-spherical particles

(Spherocylinder)

Rafik OUCHENE (LEMTA, CNRS) Anne TANIERE (LEMTA, CNRS) Mohammed KHALIJ (LEMTA, CNRS) Boris ARCEN (LRGP, CNRS)

Coimbra, 6-8 March 2013. International workshop

“Fibre Suspension Flow Modelling”

French program ANR PLAYER

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1. Introduction 2. Literature overview 3. Numerical simulation overview 4. Results 5. Conclusions 6. Future Plans 7. References

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Coal Combustion

Dispersion of Pollutants

Separation Process (cyclone)

Applications

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Context and Objectives

• This work is a part of program research about non-spherical particle dispersion. We are interested in simulating a dispersed two-phase flow using Direct Numerical Simulation under point force approximation.

• Before, we want to examine the force acting on each particle

in order to choose or develop a model that will later be introduced in the DNS.

• To verify the ability of the CFD code to give the accurate results of hydrodynamic forces acting on non-spherical particles

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Literature overview

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Variation of the drag coefficient as a function of the Reynolds number for a spherical particle (Pr Ahmadi, Clarkson University)

(1):Stokes regime (2):Intermediate regime (3):Newton regime (4):Trans-critical regime

Spherical particle

νp

p

udRe =

What’s about non-spherical particles?

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P

DD

Au

FC2

21 ρ

=22

421

p

LL

du

FC πρ=

32

1621

p

PT

du

TC πρ=

Drag coefficient Lift coefficient Torque coefficient

FD: Drag force FL : Lift force TP : Torque force Ap: Projected area u : Fluid velocity dp: Particle diameter ρ : Fluid density

Eulerian-Lagrangian methods for Two-Phase Flows

( )

( )

( ) ''''''

'

''''''

'

''''''

'

zyxyxz

z

yxzxzy

y

xzyzyx

x

LIFTDRAGp

p

TIIdt

dI

TIIdt

dI

TIIdt

dI

FFdtvd

m

=−−

=−−

=−−

+=

ωωω

ωωω

ωωω

7

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Correlation for arbitrary shaped particles 1.Ganser [1993] 2.Haider and Levenspiel [1989] 3.Hartman [1994] 4.Chien [1994] ( 5.Swamme and Ojha [1991] Pe

rfor

man

ce

Correlation for specific shaped particles •Brenner [1963] •Bowen and Masliyah [1973] •Tripathi et al [1994] •Militzer et al [1989] •Huner and Hussey [1977] •Ui et al [1984] •Michael [1966] •Shail and Norton [1969] •Davis [1990]

C H ABRA 1999

Spheroid

Cylinder

Disc

Before After

Correlation for arbitrary shaped particles 1.Holzer and Sommerfeld[2008] 2.Tran-Cong et al. [2004]

Correlation for specific shaped particles •Zastawny et al.[2012] •Loth [2008] •Yow [1994] •Vakil and Green[2011] •Mando and Rosendahl [2010]

Literature review (Drag coefficient)

The correlations must take into account: Particle shape. Particle orientation. Particle rotation.

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Relevant parameters

νeq

p

ud=Re

Particle Reynolds number is calculated using the diameter of the equivalent sphere (deq )

Sphericity (φ ) is the ratio between the surface of sphere with the same volume as the particle and the surface area of the actual particle (S):

Sdeq

2πφ =

Aspect ratio (w) is the ratio between the length (a) of the particle and its width(b):

baw =

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( )

+++=φφφφ

φ 110*42.01Re31

Re161

Re8 2.0log4.0

43DC

Arbitrary shaped particles:

Holzer and Sommerfeld[2008]

Specific shaped particles:

cbaCD ++=ReRe

( )

( ) ( ) 1098

765

42

86

42

0

ReRe31

7590,

310,

0,90,90,

cossinReRe

ReRe

ReRe

:sin

bb bbbbaaL

aaD

aaD

aDDDD

bbC

aaC

aaC

WhereCCCC

++

°=

°=

°=°=°=

−=

−=

−=

−+=

θθ

θ

θ

θ

θθθ

Zastawny et al.[2012] Rosendahl et al.[2010]

Recent correlations Formula commonly admitted:

10

( )

results nscorrelatioor alexperimentfromdeterminedare

:sin

90,

0,

30,90,90,

−+=

°=

°=

°=°=°=

θ

θ

θθθ θ

D

D

DDDD

CC

WhereCCCC

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Numerical simulation overview

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Governing equations and solutions parameters on ANSYS FLUENT

• Second-order solver for the three-dimensional Navier-Stokes equations.

•Laminar viscous model. Steady simulation. •The SIMPLE algorithm (Semi Implicid Method for Pressure-Linked Equations) is used.

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( ) upuutu

u

∆+∇−=∇⋅+∂∂

=⋅∇

νρ1

0

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Characteristics and parameters of the simulation

Particle:

Spherocylinder particle •0° ≤ θ≤ 90° •Axis ratio (b/a)=5 •Fixed and rigid particle

•Uniform flow •0.1 ≤ Rep ≤ 300

Flow: θ

13

u

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The domain and boundary conditions

Velocity-Inlet

Case : Uniform flow

Moving no-slip wall boundary condition

Pressure outlet

FD

FL

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Results of numerical simulation ANSYS-FLUENT

Uniform flow at Rep =10 and Rep =300

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Drag coefficient

Comparison with Correlations: Zastawny et al[2012]; Holzer and Sommerfeld[2008]; Rosendahl [2010]. DNS (immersed boundary method):

Zastawny et al[2012].

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Comparison at Rep =10

A similar tendency is noted for our results and those given by Zastawny et al. (CDmax / CDmin ≈ 1.75), a deviation of 30% is observed.

φ =0.69

w=5/1

Spherocylinder

Inflexion point

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Results of DNS of Zastawny et al.[2012]

Comparison of the drag and lift coefficients obtained from Brenner (1963) with the results issued from DNS of Zastawny for two ellipsoids at Re<0.1 At low Reynolds DNS of Zastawny under-predict CD compared to the theorical results

of Brenner.

φ =0.88

w=5/2

Ellipsoid 1

φ =0.99

w=5/4

Ellipsoid 2

Under-prediction of the CD at low Reynolds number by DNS Zastawny compared to theorical results. Deviation 14%

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Comparison at Rep =300

φ =0.69

w=5/1

Spherocylinder

A similar trend is noted for our results and those given by Zastawny et al. (CDmax / CDmin ≈ 4.2). The difference is lower than 10%.

Inflexion point

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Lift coefficient

Comparison with Correlations: Zastawny et al[2012]; Hoener[1963]. DNS (immersed boundary method):

Zastawny et al[2012].

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Comparison at Rep =10

φ =0.69

w=5/1

Spherocylinder

A similar tendency is noted for our results and those given by Zastawny et al. The deviation is the same to those of the drag coefficient 30%.

θθ cossin2=D

L

CCHoener correlation:

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Comparison at Rep =300

φ =0.69

w=5/1

Spherocylinder

A similar trend is noted for our results and those given by Zastawny et al. The difference is less than 2%.

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Torque coefficient

Comparison with Correlation: Zastawny et al[2012].

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Comparison at Rep =10

The torque in the Z direction given by Zastawny et al. is significantly lower than the one extracted from our simulations. Deviation ≈ 179%

φ =0.69

w=5/1

Spherocylinder

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Comparison at Rep =300

The torque in the Z direction given by Zastawny et al. is significantly lower than the one extracted from our simulations. Deviation ≈ 174%.

φ =0.69

w=5/1

Spherocylinder

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Flow visualization at Rep=10 ANSYS FLUENT

θ=90° θ=60°

θ=30° θ=0°

No recirculation zone

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θ=0° θ=30°

θ=60° θ=90°

Flow visualization at Rep=300 ANSYS FLUENT recirculation zone

Symmetry is not broken recirculation zone

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Comparison between ellipsoid and spherocylinder at Rep=300

Beginning of the dissymmetry

Symmetry •The same aspect ratio does not give the same behavior of the flow.

•The symmetry of the streamlines is not broken.

•The critical Reynolds number is not the same for both particles even if it has the same aspect ratio.

Spherocylinder

Ellipsoid w=5/1

w=5/1

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• The present results show some significant differences at low Reynolds number for CD and CL with DNS of Zastawny.

• The present torque coefficients are not in good accordance with the results of Zastawny.

• Not enough results in order to conclude about the pertinence of the existing estimations of the hydrodynamic forces (spherocylinder and ellipsoid).

The difficulty remains again in the choice of the correlation for

spherocylinder particles in order to model the motion of non spherical particles.

Conclusion

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• We will determine which is the critical Reynolds number for a spherocylinder.

• Simulation with an other type of the particles.

Future plans

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References [1] Hölzer, A and Sommerfeld, M. 2008. New simple correlation formula for the drag coefficient of non-spherical particles. Powder Technol, 184, 361-365 [2] Zastawny, M., Mallouppas, G., Zhao, F., van Wachem, B. 2011. Derivation of drag and lift force and torque coefficients for non-spherical particles in flows. International Journal of Multiphase Flow. 39, 227-239 [3] Mando, M and Rosendahl, L. 2010. On the motion of non-spherical particles at high Reynolds number. Powder Technology, 202, 1–13

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ANNEXE

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Comparison between DNS of Zasatwny and the ANSYS FLUENT simulation

φ =0.69

w=5/1

Spherocylinder

Rep =10

Rep =300

Better accordance at Re=300

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Comparison between existing correlations and the ANSYS FLUENT simulation

There is an important difference between our results and those by Zastawny. We think that is due to under-prediction of the forces on theirs simulations and this allowed for the three coefficients CD, CL and CM. Other studies must be done, using other code CFD code for this type of the particle.

φ =0.69

w=5/1

Spherocylinder

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Comparison between existing correlations and the ANSYS FLUENT simulation

Inflexion point

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φ =0.69

w=5/1

Spherocylinder

We have the same tendency between our results and those of Zastawny at the both Reynolds number. But at Re=10 the results of Zastawny tend to under-precdict CD than us, as we seen for the ellipsoid at Re=0,1.

Rep =300

Rep =10

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Comparison between existing correlations and the ANSYS FLUENT simulation

We have the same tendency between our results and those of Zastawny at the both Reynolds number. But at Rep =10 the results of Zastawny tend to under-precdict CD than us, as we seen for the ellipsoid at Rep =0,1.

φ =0.69

w=5/1

Spherocylinder

Rep=10

Rep=300

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