Multiphase CFD Applied to Steam Condensation Phenomena in...
Transcript of Multiphase CFD Applied to Steam Condensation Phenomena in...
Multiphase CFD Applied to Steam Condensation Phenomena in the
Pressure Suppression Pool
Marco Pellegrini
STAR Japanese Conference 2016Yokohama, Japan – June 9th 2016
N U P E C
6/10/2016 STAR Japanese Conference, Yokohama, Japan
NUCLEAR PLANTS AFFECTED BY THE 3.11 EARTHQUAKE 2
Fukushima Daiichi
Fukushima Daini
Onagawa
Operating reactor
Under inspection
~ 130 kmJMA seismic intensity
March 11th 2011
6/10/2016 STAR Japanese Conference, Yokohama, Japan
STATION BLACK OUT 3
R/B
High Pressure Alternate Cooling system
Reactor Core Isolation Cooling system
Courtesy of A. Obonai, Tohoku Electric Power CO
RCIC quencherExperiment at SIET, Italy (IAE)
T-quencherExperiment at SIET, Italy (IAE)
6/10/2016 STAR Japanese Conference, Yokohama, Japan
DIRECT CONTACT CONDENSATION IN S/C 4
R/B
MAKE-UP WATER SYSTEMSDIRECT CONTACT CONDENSATION
6.E+06
6.E+06
7.E+06
7.E+06
7.E+06
7.E+06
7.E+06
8.E+06
0 500 1000 1500 2000 2500 3000 3500
RPV pressure [M
Pa(abs)]
Time(s)
Computation by A. Buccio(IAE), 2016
Injectionpoint
~ 30 m
6/10/2016 STAR Japanese Conference, Yokohama, Japan
EULERIAN TWO-PHASE FLOW 5
∙ ∙
∙ , ∙ ∙ ∙
Instantaneous representationH
eat f
lux
Source terms ∆ ∆ Energy equation
Average representation
Hea
t flu
x
6/10/2016 NURETH-16, Hyatt Regency, Chicago
HEXAHEDRAL MESH APPLIED TO A SPHERE 6
DArea Density Magnitude of Volume
Fraction Gradient
D/16 D/32 D/64 D/128
D
Volume Fraction
6/10/2016 NURETH-16, Hyatt Regency, Chicago
HEXAHEDRAL MESH APPLIED TO A SPHERE 7
0.0%2.0%4.0%6.0%8.0%
10.0%12.0%14.0%16.0%18.0%20.0%
d/8 d/16 d/32 d/64 d/128
Erro
r [%
]
~ 9% error with large refinement
D/16 D/32 D/64 D/128
Error between the computed and theoretical area
D
6/10/2016 NURETH-16, Hyatt Regency, Chicago
POLYHEDRAL MESH APPLIED TO A SPHERE 8
D/16 D/32
0.00%
0.50%
1.00%
1.50%
2.00%
2.50%
3.00%
3.50%
d/16 d/32 d/64 d/128
Erro
r [%
]
D/8Error between the computed and theoretical area
~ 2.5% error with large refinement
6/10/2016 STAR Japanese Conference, Yokohama, Japan
DOMAIN AND MESH STRATEGIES 9
Small nozzle diameterD = 2 mm
Large nozzle diameterD = 210 mm
Mesh elements: 305,067
6/10/2016 STAR Japanese Conference, Yokohama, Japan
DOMAIN AND MESH STRATEGIES 10
Mesh elements: 405,067
D/16
Small nozzle diameter Large nozzle diameter
Mesh elements: 305,067
Small nozzle diameterD = 2 mm
Large nozzle diameterD = 210 mm
6/10/2016 STAR Japanese Conference, Yokohama, Japan
MESH SENSITIVITY - 1 11
0.0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0 20 40 60 80 100 120
Inte
rfaci
al a
rea
[cm
2 ]
Time [ms]
IFA [Mesh X 0.5]IFA [Mesh X 0.75]IFA [Mesh x1.0]IFA [Mesh x1.25]
MESH x1.25 MESH x1.0 MESH x0.750 MESH x0.5
Interfacial area
6/10/2016 STAR Japanese Conference, Yokohama, Japan
DIRECT CONTACT CONDENSATION: CHUGGING 12
Single hole pipe
In recent experiment we employed transparent pipes to visualize the bubble phenomenology during direct contact condensation
Pressure sensor
0.231 m
6/10/2016 Severe Accident Mitigation and Research Collaboration
EXPERIMENTAL EVIDENCEPo
ol te
mpe
ratu
re [°
C]
TPOOL = 57-61 °C
Steam reaching point
0.2 kg/s
water level
2.8
m
1.24
m
13
6/10/2016 STAR Japanese Conference, Yokohama, Japan
DIRECT CONTACT CONDENSATION: CHUGGING-2 14
pressure sensorMulti hole pipe
In recent experiment we employed transparent pipes to visualize the bubble phenomenology during direct contact condensation
NURETH-16, Hyatt Regency, Chicago
RAYLEIGH-TAYLOR INSTABILITY
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15
Psteam < Pwater
2
1i ska
Final terms for area growth
A
steam
water
Psteam
PwaterPsteam Pwater
steam
water
Accelerating flow field
Psteam
Pwater
n tt t te
6/10/2016 STAR Japanese Conference, Yokohama, Japan
IMPLEMENTATION INTO STAR-CCM+ 16Compressible steam flow Compressible steam flow
Record amplitude length at previous time step
6/10/2016 STAR Japanese Conference, Yokohama, Japan
LARGE NOZZLE DIAMETER: POOLEX 17
WATER• Incompressible – Constant properties• k-ε standard• Temperature = 62 ºCSTEAM• Compressible
velocity inletpressure outlet
adiabaticwalls
T = 106 °Cv = 11.02 m/s
Time step = Courant number limitedStopping criteria at interfacial mass transfer (1% of inlet mass flow rate)
Mesh elements: 405,067
D/16
6/10/2016 STAR Japanese Conference, Yokohama, Japan
EFFECT OF RTI MODELIZATION 18
Pressuremonitor
6/10/2016 STAR Japanese Conference, Yokohama, Japan
VOLUME FRACTION 19
Tpool = 62 ºCTpool = 62 ºC
Minimum area model Rayleigh-Taylor Instability Model
Steam flow Steam flow
6/10/2016 STAR Japanese Conference, Yokohama, Japan
20
EXP
RTI model
Tanskanen, Ph.D. Thesis 2012
No RTI model
6/10/2016 NURETH-16, Hyatt Regency, Chicago
EFFECT OF MISPREDICTION OF CHUGGING 21
Prediction of oscillating bubble creates thermal stratification in the pool
Chugging is responsible for very large mixing in the pool
6/10/2016 STAR Japanese Conference, Yokohama, Japan
SMALL NOZZLE DIAMETER: CLERX ET AL. 22
WATER• Incompressible – Constant properties• k-ε standard• Temperature = 25 ºCSTEAM• Compressible
Time step = Courant number limitedStopping criteria at interfacial mass transfer (1% of inlet mass flow rate)
Mesh elements: 405,067
D/16
6/10/2016 STAR Japanese Conference, Yokohama, Japan
VOLUME FRACTION FIELD 23
Minimum area model Rayleigh-Taylor Instability Model
Clerx et al., 20090.3 ms 0.6 ms
1.2 ms
0.9
1.5 ms 1.8 ms
Bubble implosion is less than 2 ms in the experiment at it appears immediately
6/10/2016 STAR Japanese Conference, Yokohama, Japan
CLERX ET AL. EXPERIMENT 24
0.0
1.0
2.0
3.0
4.0
5.0
6.0
0 2 4 6 8 10 12
Pene
tratio
n Le
ngth
[mm
]
Time [ms]
Clerx ExperimentBL + no RTIRTI
Minimum area model RTI ModelClerx et al., 2009
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PREDICTION OF TEMPERATURE DISTRIBUTION 25
RTI Model
Clerx et al., 2009
Measured temperature field
Minimum area model
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THE CHALLENGE OF ACCIDENT COMPUTATION 26
R/B R/B R/B
accident time scale [days]
Unit 1 vent pipes Unit 2 RCIC Unit 3 RCIC
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UNIT 3UNIT 2
UNIT 1
Courtesy of S. Mizokami, TEPCO
Fukushima Daiichi power plantwhat are the conditions at this moment?