C. Lifante, T. Frank, A. Burns ANSYS [email protected] 1 D inj= 4mm Source point @...

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Prediction of Polydisperse Steam Prediction of Polydisperse Steam Polydisperse Steam Bubble Condensation in Subcooled Water using th Ih Polydisperse Steam Bubble Condensation in Subcooled Water using th Ih the Inhomogeneous MUSIG Model the Inhomogeneous MUSIG Model C. Lifante, T. Frank, A. Burns ANSYS [email protected] C. Lifante, T. Frank, A. Burns ANSYS [email protected] [email protected] D. Lucas, E. Krepper Forschungszentrum [email protected] D. Lucas, E. Krepper Forschungszentrum © 2009 ANSYS, Inc. All rights reserved. 1 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. 1 ANSYS, Inc. Proprietary Forschungszentrum Dresden-Rossendorf Forschungszentrum Dresden-Rossendorf

Transcript of C. Lifante, T. Frank, A. Burns ANSYS [email protected] 1 D inj= 4mm Source point @...

Page 1: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Prediction of Polydisperse Steam

Prediction of Polydisperse Steam Polydisperse Steam

Bubble Condensation in Subcooled Water using

th I h

Polydisperse Steam Bubble Condensation in Subcooled Water using

th I h the Inhomogeneous MUSIG Model

the Inhomogeneous MUSIG Model

C. Lifante, T. Frank, A. BurnsANSYS

[email protected]

C. Lifante, T. Frank, A. BurnsANSYS

[email protected]@ansys.com

D. Lucas, E. KrepperForschungszentrum

[email protected]

D. Lucas, E. KrepperForschungszentrum

© 2009 ANSYS, Inc. All rights reserved. 1 ANSYS, Inc. Proprietary© 2009 ANSYS, Inc. All rights reserved. 1 ANSYS, Inc. Proprietary

Forschungszentrum Dresden-RossendorfForschungszentrum Dresden-Rossendorf

Page 2: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Outline

• Motivation• Model descriptionp• Validation

– TOPFLOW facility & condensation experimentTOPFLOW facility & condensation experiment– CFD Experiment comparison

• Previous approaches vs. extended MUSIG pp• Improvements in the extended MUSIG simulations

• Summary & conclusions

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Page 3: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Outline

• Motivation• Model descriptionp• Validation

– TOPFLOW facility & condensation experimentTOPFLOW facility & condensation experiment– CFD Experiment comparison

• Previous approaches vs. extended MUSIG pp• Improvements in the extended MUSIG simulations

• Summary & conclusions

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Page 4: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Motivation

• NRS applications:– Subcooled boiling in nucl. react fuel assemblies– Steam injection into pools– Steam bubble entrainment in subcooled liquids

by impinging jets

C d / t d d IAD• Cond./evap. rates depend on IAD bubble size distributionNeed of polydispersed• Need of polydispersedinhomogeneous simulations

• Need to deal with phase

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• Need to deal with phase change effects

Page 5: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Outline

• Motivation• Model descriptionp• Validation

– TOPFLOW facility & condensation experimentTOPFLOW facility & condensation experiment– CFD Experiment comparison

• Previous approaches vs. extended MUSIG pp• Improvements in the extended MUSIG simulations

• Summary & conclusions

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Page 6: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Standard Inhomog. MUSIG Model

• Polydisperse fluids •Small bubbles move with the fluid phase

d1 d3 d4 d5 d6 d7 d8d2•Large bubbles are more influenced by

v1 v2 v3

buoyancy

•Lift coefficient changes its sign at a critical size;depends on (p T)Velocity group mass transfer

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depends on (p,T)

Break up Coalescence

Page 7: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Standard Inhomog. MUSIG Model

• MUSIG setup:– Definition of the initial diameter classes (di)

• Mass classes used – Definition of velocity groups (vj)

• Homogeneous/Inhomogeneous• Which di belong to each vj

– 1 size fraction equation for each bubble diameter

– 1 momentum equation for each velocity group

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Page 8: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Model Extension description

• Basic population balance equationsNew terms

dn(m, r, t) n(m, r, t) U(m, r, t)n(m, n(m, r, t) m(r, t)dt

r, t)m tt r

B D B D

• Size fraction equations

B B C CB D B D Bubble number density

Breakup/Coalescence terms

Size fraction equations

B B C C

ji d i i d i i B D B Dj i( r f ) ( r U f ) S S S S

t xS

i ii i 1

i i 1 i 1 i

m mm m m m

Si=

for evaporation

≈≈© 2009 ANSYS, Inc. All rights reserved. 8 ANSYS, Inc. Proprietary

i ii 1 i

i i 1 i 1 i

m mm m m m

Si

for condensation iii

i

ii ≈≈

Page 9: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Outline

• Motivation• Model descriptionp• Validation

– TOPFLOW facility & condensation experimentTOPFLOW facility & condensation experiment– CFD Experiment comparison

• Previous approaches vs. extended MUSIG pp• Improvements in the extended MUSIG simulations

• Summary & conclusions

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Page 10: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

TOPFLOW Test Facility @ FZD8m

L~ 8

D=195mm

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Courtesy of FZD

Page 11: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Condensation Test Case

• P=2 [MPa]• Jw=1.0 [m/s]• Js=0.54 [m/s]s [ ]• Ts=214.4 [C]• Tw=210.5 [C] ∆Tw=3.9 [K]Tw 210.5 [ C] ∆Tw 3.9 [K]• Dinj = 1 [mm]• Detailed experimental data:Detailed experimental data:

– Bubble size distributionRadial steam volume fraction distribution

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– Radial steam volume fraction distributionDirk Lucas, Horst-Michael Prasser: “Steam bubble condensation in sub-cooled water in case of co-current vertical pipe flow”,Nuclear Engineering and Design, Volume 237, Issue 5, March 2007, Pages 497-508

Page 12: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Condensation Test Case

E i t l di l

Experimental bubble size distribution

Experimental radial vapor distribution

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Page 13: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Numerical Setup

• 1/6 of geometry simulated, 60• Symmetry b.c.• 260.442 elements*• 12 x Injection nozzles modeled

by SOURCE POINTS– Dinj modified (4mm) for vinj

• SST turbulence model• Fdrag, Flift, FTD considered

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Page 14: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Physical Model Setup

• Locally Monodisperse– Particle diameter: constant number of bubbles

dP=dP(dP|Inlet, NP|Inlet)• Standard MUSIG & Extended MUSIG

– 25 bubble size classes– 3 velocity groups:

03 [mm],36 [mm], 630 [mm]– Break up model: Luo & Svendsen (FB=0.025)– Coalescence model: Prince & Blanch (FC=0.05)

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C

Page 15: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Results: Vertical averaged steam distribution

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Injection nozzles Pipe end

Page 16: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Results: Radial steam distribution

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Page 17: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Results: Radial steam distribution

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Page 18: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Results: Bubble size distribution

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Page 19: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Results: Bubble size distribution

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Page 20: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Results: Tests Comparison

Config 1

Config 2

Config 3

Config 2

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Page 21: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

TOPFLOW Condensation case

Config 1 Dinj = 4mm Source point @ W ll - - -Config 1 Dinj 4mm Wall

Config 2 Dinj= 4 mm Source point @ 75 mm FWLF CTD=1.5 Nu=2+0.15Rep

0.8Pr0.5

Config 3 Dinj= 1 mm Source point @ 75 mm FWLF CTD=1.5 Nu=2+0.15Rep

0.8Pr0.5

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Page 22: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Results: Vapor Volume Fraction

© 2009 ANSYS, Inc. All rights reserved. 22 ANSYS, Inc. ProprietaryConfig 2 Config 3Config 1

Page 23: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Results: Vertical averaged steam distribution

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Page 24: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Results: Radial steam distribution

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Page 25: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Results: Radial steam distribution

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Page 26: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Results: Bubble size distribution

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Page 27: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Results: Bubble size distribution

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Page 28: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Outline

• Motivation• Model descriptionp• Validation

– TOPFLOW facility & condensation experimentTOPFLOW facility & condensation experiment– CFD Experiment comparison

• Previous approaches vs. extended MUSIG pp• Improvements in the extended MUSIG simulations

• Summary & conclusions

© 2009 ANSYS, Inc. All rights reserved. 28 ANSYS, Inc. Proprietary

y

Page 29: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Summary & Conclusions

• An extension of the MUSIG model in ANSYS CFX in order to catch phase change effect was implemented

• Condensation case at the TOPFLOW geometry used for validationfor validation

• The comparison with previous approaches proved the necessity of the extension

• Qualitatively better results, however improvements in the Setup were requiredA parameter study led to also quantitative• A parameter study led to also quantitative satisfactory results

• Implementation performed in a customized solver

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p pbased on ANSYS CFX 12

Page 30: C. Lifante, T. Frank, A. Burns ANSYS conxita.lifante@ansys...Config 1 D inj= 4mm Source point @ Wll-- - Wall Config 2 D inj=4 mm Source point @ 75 mm F WLF CTD=1.5 Nu=2+0.15Re p 0.8Pr0.5

Th k Y !Thank You!© 2009 ANSYS, Inc. All rights reserved. 30 ANSYS, Inc. Proprietary