Transcript TUSTP

TUSTP 2003 Mechanistic Modeling and CFD Simulations of Oil-Water Dispersions in Separation Components

by Carlos F. Torres May 20, 2003

Topics

Background

Objectives

Particle Tracking Model

Preliminary Results

Universal Dispersion Model

Background

Knowledge of particle motion and phase distribution enhance performance evaluation of separation equipment will

TUSTP has used the Eulerian-Lagrangian technique to design and analyze performance of separation devices such as GLCC, LLCC and LLHC

Existing models carry out simulations considering mainly the following forces acting on a particle: drag and buoyancy

Additionally, these models assume particle local equilibrium

Objectives

The general objectives of this study are to develop models capable of characterizing hydrodynamics of multiphase dispersion flow in separations and piping components

Initially, study focuses on dilute and dense dispersed flow

Develop a mechanistic model for calculating droplet motion, considering the different acting forces

Determine dispersed phase void fraction

Validate and extend the three way coupling approach proposed by Gomez 2001

Particle Tracking Model

General approach

Simplified approach

Future improvements

Particle Tracking: General Approach

Gomez 2001 presented a new Eulerian – Lagrangian mechanistic model:

Local equilibrium assumed for dispersed phase

Forces used: drag, lift, body force, added mass and pressure gradient

Model is one way coupling between continuous and dispersed phase, considering variation of interfacial area

Lagrangian Equation

Forces on particle

m p d V

dt

 

F d

 

F l

 

F b

 

F m

 

F p

 

F other

  0 

Effects of continuous phase turbulence on particle:

Behzadi et al (2001) presented an averaging approach for the effects of fluid turbulence on particles

Iliopoulos et al. (2003) presented a stochastic model for the effects of turbulence in dispersed flow

Particle Tracking: Simplified Approach

Modifications of Gomez model (2001):

Forces considered: drag, lift and body force

Main goal is calculation of particle trajectory

Parametric technique (function of time) allows determination of particle’s residence time (integration 2 nd order accuracy)

Particles are spherical and non-deformable, particle to particle interaction not considered (dilute dispersion)

One way coupling

3D solution developed for Cartesian and Cylindrical coordinate systems

Modified Gomez Model

Forces on Particle

 0  

F d

 

F l

 

F b

Particle Position

x i

 1 

x i

ti

 

ti 1 V x dt y i

 1 

y i

ti ti

 

1 V y dt z i

 1 

z i

ti ti

 

1 V z dt

Particle Tracking: Future Improvements

  

Extend model capability to include:

Added mass force

Pressure gradient force (hydrodynamic)

Fluid turbulent effects

Particle transients effect Develop mechanistic model for estimation of void fraction using stochastic approach Explore limits of dilute flow assumption, and extend to dense flow

Preliminary Results

Particle Tracking in Pipe Flow

Particle Tracking in Stratified Flow

Particle Tracking in Conventional Separators

Particle Tracking: Pipe Flow

Dimensionless Velocity Profile 1 0.9

0.8

0.7

y

 Re  0.6

0.5

0.4

0.3

0.2

0.1

0 0 0.2

0.4

U

U

max Laufer, J. 1951, (Re = 40000) U+ Inner Layer U+ Outher Layer 0.8

Mixing Length Velocity Profile

1

0.06

0.04

0.02

0 -0.02

-0.04

-0.06

0

Particle Tracking: Pipe Flow

= 0 o , d = 5in, V cont = 0.01 m/s.

Water Continuous (1000 kg/m 3 , 1cp).

Dispersed phase Oil (850 kg/m 3 ), dp = 100 microns

0.5

With lift force.

Residence time = 161.53 s Without lift force. Residence time = 99.35 s 1

Pipe length [m]

1.5

2 2.5

Particle Tracking: Stratified Flow

0.04

0.02

0 

= 0 o , d = 3in, Uls = 0.1 m/s, Ugs = 1.0 m/s Air Water system at 25

C and 1 atm.

Vl [m/s] 0.350

0.325

0.300

0.275

0.250

0.225

0.200

0.175

0.150

0.125

0.100

0.075

0.050

0.025

0.000

0.04

0.02

0 dp = 25 micros dp = 50 micros liquid level   1000 kg/m 3   1.2

kg/m 3 -0.02

-0.04

-0.04

-0.02

0

X [m]

0.02

-0.02

h/d = 0.5816

hl = 0.6035

0.04

-0.04

0 1 2 3 4 5

Pipe length [m]

6

Shoham and Taitel (1984)

7 8 9

Fluent

12 Mar 2003

title

2.5

2 1.5

1

Fluent 6.0

Oil density = 850 kg/m 3 viscosity = 30 cp Velocity at the inlet = 2 m/s at the interphase = 0.2 m/s Diameter at the inlet = 0.1 m at the outlet = 0.1 m Vessel liquid level = 1 m Reynolds Number at the inlet = 5666.7

in the vessel = 5666.7

0.5

Velocity Magnitude 2.600E+00 2.463E+00 2.326E+00 2.189E+00 2.053E+00 1.916E+00 1.779E+00 1.642E+00 1.505E+00 1.368E+00 1.232E+00 1.095E+00 9.579E-01 8.211E-01 6.842E-01 5.474E-01 4.105E-01 2.737E-01 1.368E-01 0.000E+00 0 -1 -0.5

0 1 1.5

2 2.5

3

Conventional Separators

12 Mar 2003 title Vessel Oil density = 850 kg/m 3 Velocity at the inlet = 2 m/s at the interphase = 0.2 m/s Diameter at the inlet = 0.1 m at the outlet = 0.1 m Vessel liquid level = 1 m Reynolds Number at the inlet = 5666.7

in the vessel = 5666.7

Velocity Magnitude 2.600E+00

Vessel 2D

12 Mar 2003

Vessel

2.5

2 1.5

1

Vessel 2D v1.0

Oil density = 850 kg/m 3 viscosity = 30 cp Velocity at the inlet = 2 m/s at the interphase = 0.2 m/s Diameter at the inlet = 0.1 m at the outlet = 0.1 m Vessel liquid level = 1 m Reynolds Number at the inlet = 5666.7

in the vessel = 5666.7

0.5

0 0 0.5

1 1.5

2

x [m]

2.5

3 3.5

Vel 2.600E+00 2.463E+00 2.326E+00 2.189E+00 2.053E+00 1.916E+00 1.779E+00 1.642E+00 1.505E+00 1.368E+00 1.232E+00 1.095E+00 9.579E-01 8.211E-01 6.842E-01 5.474E-01 4.105E-01 2.737E-01 1.368E-01 0.000E+00 4

Fluent

12 Mar 2003

title

2.5

2 1.5

1

Fluent 6.0

Oil density = 850 kg/m 3 viscosity = 30 cp Velocity at the inlet = 2 m/s at the interphase = 0.2 m/s Diameter at the inlet = 0.1 m at the outlet = 0.1 m Vessel liquid level = 1 m Reynolds Number at the inlet = 5666.7

in the vessel = 5666.7

0.5

 0 -1 Velocity Magnitude 2.600E+00 2.463E+00 2.326E+00 2.189E+00 2.053E+00 1.916E+00 1.779E+00 1.642E+00 1.505E+00 1.368E+00 1.232E+00 1.095E+00 9.579E-01 8.211E-01 6.842E-01 5.474E-01 4.105E-01 2.737E-01 1.368E-01 0.000E+00 -0.5

0 1 1.5

2 2.5

3

Conventional Separators

Vessel Oil density = 850 kg/m viscosity = 30 cp 3 Velocity at the inlet = 2 m/s at the interphase = 0.2 m/s Diameter at the inlet = 0.1 m at the outlet = 0.1 m Vessel liquid level = 1 m Reynolds Number at the inlet = 5666.7

in the vessel = 5666.7

Vel 2.600E+00

Vessel 2D

12 Mar 2003

Vessel

2.5

2 1.5

1

Vessel 2D v1.0

Oil density = 850 kg/m 3 viscosity = 30 cp Velocity at the inlet = 2 m/s at the interphase = 0.2 m/s Diameter at the inlet = 0.1 m at the outlet = 0.1 m Vessel liquid level = 1 m Reynolds Number at the inlet = 5666.7

in the vessel = 5666.7

0.5

0 0 0.5

1 1.5

2

x [m]

2.5

3 3.5

Vel 2.600E+00 2.463E+00 2.326E+00 2.189E+00 2.053E+00 1.916E+00 1.779E+00 1.642E+00 1.505E+00 1.368E+00 1.232E+00 1.095E+00 9.579E-01 8.211E-01 6.842E-01 5.474E-01 4.105E-01 2.737E-01 1.368E-01 0.000E+00 4

Particle Tracking: Conventional Separators

Particle Residence Time = 2.63 s Particle Density = 2500 kg/m 3 Particle Diameter = 500 micron

Particle Tracking: Conventional Separators

Frame 001

12 Mar 2003

Particle Tracking

2.5

Particle Residence Time = 2.362 s Particle Density = 2500 kg/m 3 Particle Diameter = 500 micron 2 1.5

1 0.5

0 0 1 2

X

3 4

Frame 002

12 Mar 2003

Contour Plot

2.5

2 1.5

1 0.5

0 0 1 2

X

3 Velocity Magnitud 2.6000E+00 2.4632E+00 2.3263E+00 2.1895E+00 2.0526E+00 1.9158E+00 1.7789E+00 1.6421E+00 1.5053E+00 1.3684E+00 1.2316E+00 1.0947E+00 9.5789E-01 8.2105E-01 6.8421E-01 5.4737E-01 4.1053E-01 2.7368E-01 1.3684E-01 0.0000E+00 4

Universal Dispersion Model

Gomez Model (2001)

The Eulerian field is known (average velocities, turbulent kinetic energy and energy dissipation)

Solve Lagrangian field using the proposed equation, to calculate slip velocity within flow field

Solve diffusion equation using slip velocity information, to predict void fraction distribution

Calculate bubble or droplet diameter using Eulerian turbulent quantities and void fraction distribution

Repeat non-linear process until convergence is reached

Phase Coupling Model

Definition of Phase Coupling

One-way Coupling: reverse effect.

Fluid flow affects particle while there is no

Two-way Coupling: fluid flow affects particle and vice versa.

Four-way Coupling: Additionally from above, there are hydrodynamic interactions between particles, and turbulent particle collisions.

Three-way Coupling

Phase Coupling Model

Continuous phase momentum equation (N- S Equation)

u i

t

   

j u i

x j

  1  

P

x i

   

x j

  

u i

x j

 

u j

x i

u i

    MP

so i

 T

si i

Dispersed phase momentum equation (average)

m p d V

p dt

 

F d

 

F l

 

F b

 

F m

 

F p

 

F turbulence

 

F other

Particle Source Term, MPso is estimated by coupling mass and momentum balances over control volume.

Two-way Coupling: Solution Scheme

PSI – Cell technique, Crowe et al. (1977) Huber & Sommerfelt (1997).

Air continuous Phase.

= 0 o , d = 80 mm, V = 24 m/s, Dispersed phase

d = 2500 kg/m 3 d p = 40 micron

Model Potential

LLCC Dispersion of Oil in Water with Water Layer at the Bottom V m = 0.6 m/s W.C = 67%

Questions

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