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TRACE Model Development
WORKING GROUP MEETING SPRING 2016TASK 2 BREAKOUT SESSION
ANN ARBOR, MI
Emory Brown
• Task Description
• Timeline
• Pump
• Simple Models
• Revised Geometry and Test Train Model
• Current Challenges and Questions
Outline
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Task 2.2 Overview
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Flow of information
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Commercial PWR
TREAT Reactor
TWERL Loop
Neutronic boundary conditions
Commercial PWR
Transient CHF data
TRTL Loop
Task 2.2.11: Modeling of benchmark test with TRACE
• OSU will develop a TRACE model for one of the benchmark tests performed using the U.S. NRC code TRACE. Modeling of the benchmark test will be done blindly, based on the design package put together as a part of task 2.2.3. The data will not be made available until the modeling and results have been completed.
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Task 2.2.11 specific objectives
• Start with TWERL model.
• Known geometries.
• TRTL model will be nearly identical
• Compare model with RELAP5-3D
• Finalize TRTL model
• Model benchmark simulation and compare to experimental benchmark data (2.2.13)
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TRACE Model Development Timeline
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NovOct Dec FebJan Mar Apr
Gain access to TRACE, SNAP, and AptPlot
Simple models to familiarize with code.
Gain access to TWERL Solidworks model
Gradually increase complexity and identify issues and gaps in knowledge
Found Theory and Model Guidelines manuals
Focus on test section and compare to RELAP-5
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1.5 10 · .
Pump Impeller Inertia *
118 ·
.
Pump Motor Inertia *
* Wylie et al.
Pump Information
· · ·
Flow Rate Head Efficiency Power Normalized Curve
GPM m3/s ft m m2/s2 % KW(in) KW(heat) q/ω h/ω2
0.24 1.48E‐05 59.64 18.18 178.32 0.1% 2.649 2.646 2.599E‐05 9.112E‐06
2.88 1.81E‐04 59.27 18.07 177.23 2.0% 1.610 1.578 3.179E‐04 9.056E‐06
5.88 3.71E‐04 58.78 17.92 175.75 6.0% 1.089 1.024 6.506E‐04 8.981E‐06
9.18 5.79E‐04 58.04 17.69 173.53 12.0% 0.839 0.738 1.015E‐03 8.867E‐06
13.68 8.63E‐04 56.46 17.21 168.82 18.0% 0.811 0.665 1.513E‐03 8.627E‐06
17.61 1.11E‐03 54.69 16.67 163.53 22.0% 0.827 0.645 1.947E‐03 8.357E‐06
20.86 1.32E‐03 52.73 16.07 157.66 24.0% 0.866 0.658 2.307E‐03 8.057E‐06
RATED 25.03 1.58E‐03 50.14 15.28 149.93 26.0% 0.912 0.675 2.768E‐03 7.661E‐0629.24 1.84E‐03 47.81 14.57 142.96 27.5% 0.961 0.697 3.233E‐03 7.305E‐06
31.65 2.00E‐03 45.99 14.02 137.50 27.8% 0.990 0.714 3.500E‐03 7.026E‐06
33.72 2.13E‐03 43.96 13.40 131.44 27.8% 1.008 0.728 3.729E‐03 6.717E‐06
37.10 2.34E‐03 41.11 12.53 122.93 27.5% 1.048 0.760 4.103E‐03 6.282E‐06
40.36 2.55E‐03 38.64 11.78 115.53 26.7% 1.104 0.809 4.463E‐03 5.904E‐06
42.10 2.66E‐03 37.13 11.32 111.02 26.1% 1.132 0.836 4.655E‐03 5.673E‐06
44.03 2.78E‐03 35.17 10.72 105.17 25.5% 1.148 0.855 4.868E‐03 5.374E‐06
46.78 2.95E‐03 32.12 9.79 96.03 24.5% 1.159 0.875 5.172E‐03 4.907E‐06
50.07 3.16E‐03 27.87 8.49 83.33 23.5% 1.122 0.858 5.536E‐03 4.258E‐06
gc 9.81m/s2 QR 1.58E‐03 m3/sS.G. 1 [unitless] HR 149.93 m2/s2
RPM3450RPM 5.790 in‐lbf ΩR 361.3 rad/sec361 rad/sec 0.482 ft‐lbf HPR, liquid 0.316945556 hp
Impeller Size 3.5 in 0.654 kg‐m2/s2 τR 0.654173293 Pa‐m3
IP 1.04E‐03 kg‐m2
IM 5.98E‐04 kg‐m2
Effective M.O.I 1.6350E‐03 kg‐m2
Pump Information
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Pump Information
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0%
5%
10%
15%
20%
25%
30%
0 10 20 30 40 50 60
Head
[ft]
Flow Rate [GPM]
Pump Curve ‐ 3.5" Impeller @ 67 Hz
Head
Efficiency
Simple loops…
• Learning the ropes of TRACE, SNAP, and APTPLOT. • Creating incrementally complex heated water loops to verify
solutions to analytical thermal hydraulic problems.
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t[s]=m kg
Q kJs
CpkJ
kg K∆T K
4.619782.31173 4.18 12
99.83
Creating a TRACE model of TWERL• Extract physical dimensions from
Solidworks model. • Pump information provided from
vendor pump curve. • Translate into TRACE model• Run initial case similar to simplified
model. Q=(m/t)(Cp)(∆T)
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4/21: Model revamp with lessons learned
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AA
0.076200 m
0.340030 m
0.021819 m
0.027051 m
0.027864 m
0.024689 m
0.027864 m 0.026848 m
0.057150 m 0.005715 m
SECTION A-ASCALE 1 : 2
AA
0.136624 m
0.223510 m
0.079055 m
C
A
B
SECTION A-ASCALE 1 : 2
0.003200 m
DETAIL CSCALE 2 : 1
Top of 3rd Section
0.003200 m
DETAIL ASCALE 2 : 1
Bottom of 1st Section
0.003200 m DETAIL B
SCALE 2 : 1
Bottom of fueled section.Top is the top of the last pellet
0.052502 m
0.039051 m
0.026645 m
0.025425 m
0.024549 m
0.116442 m
Test Section Geometry
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Comp. Cell Length (m) dZ (m) In Edge Flow Area (m2) HD (m) Out Edge Flow Area
(m2) HD (m) Changing Diameter?
Annular? Dinner (m) Douter
(m) VolumeVolume
average flow area
110
1 0.0762 0.0762 1 0.00057472 0.027051 2 0.00057472 0.027051 0 4.37937E‐05 0.0005747202 0.34003 0.34003 2 0.000609785 0.027864 3 0.000609785 0.027864 0 0.000207345 0.0006097853 0.021819 0.021819 3 0.000478737 0.024689 4 0.000478737 0.024689 0 1.04456E‐05 0.0004787374 0.026848 0.026848 4 0.000609785 0.027864 5 0.000609785 0.027864 0 1.63715E‐05 0.0006097855 0.05715 0.05715 5 0.000248287 0.01778 6 0.000216617 0.005715 1 X 0.00635 0.01778 0.000247683 0.004333917
120 1 0.329828 0.329828 1 0.000127286 0.003188 2 0.000127286 0.003188 0 X 0.009526 0.0159 4.19824E‐05 0.000127286
1211 0.136624 0.136624 1 0.000127674 0.0032 2 0.000127674 0.0032 0 X 0.00950 0.01590 1.74434E‐05 0.0001276742 0.22351 0.22351 2 0.000127674 0.0032 3 0.000127674 0.0032 0 X 0.00950 0.01590 2.85365E‐05 0.0001276743 0.079055 0.079055 3 0.000127674 0.0032 4 0.000127674 0.0032 0 X 0.00950 0.01590 1.00933E‐05 0.000127674
122
1 0.441325 0.441325 1 0.000137688 0.003393 2 0.000137688 0.003393 0 X 0.009524 0.01631 6.07651E‐05 0.000137688
2 0.022225 0.022225 2 0.000071601 0.001981 3 0.000546175 0.008784 1 X * See attached figure 6.20899E‐06 0.000279370
3 0.069056 0.069056 3 0.000387948 0.022225 4 0.000387948 0.022225 0 2.67901E‐05 0.000387948123 1 0.572294 0.572294 1 0.000507705 0.025425 2 0.000507705 0.025425 0 0.000290557 0.000507705
130
1 0.0257285 0.0257285 1 0.000507705 0.025425 2 0.002164919 0.052502 1 3.19121E‐05 0.0012403412 0.026645 0.026645 2 0.002164919 0.052502 3 0.002164919 0.052502 0 5.76843E‐05 0.0021649193 0.1031195 0.1031195 3 0.002164919 0.052502 4 0.002164919 0.052502 0 0.000223245 0.0021649191 0.024549 1 0.000557598 0.026645 2 0.000557598 0.026645 0 1.36885E‐05 0.000557598
131 1 0.50165 0.50165 1 0.002123227 0.051994 2 0.002123227 0.051994 0.001065117 0.002123227
140
1 0.023749 1 0.000557598 0.026645 2 0.000557598 0.026645 0 1.32424E‐05 0.0005575982 0.0598473 2 0.000557598 0.026645 3 0.000557598 0.026645 0 3.33707E‐05 0.0005575983 0.060541 0.060541 3 0.000557598 0.026645 4 0.000557598 0.026645 0 3.37576E‐05 0.0005575984 0.020231 0.020231 4 0.000478737 0.024689 5 0.000478737 0.024689 0 9.68533E‐06 0.0004787375 0.103308 0.103308 5 0.000609785 0.027864 6 0.000609785 0.027864 0 6.29957E‐05 0.0006097856 0.021819 0.021819 6 0.000478737 0.024689 7 0.000478737 0.024689 0 1.04456E‐05 0.000478737
1501 1.692453 1.692453 1 0.000609785 0.027864 2 0.000609785 0.027864 0 0.001032033 0.0006097852 0.021819 0.021819 2 0.000478737 0.024689 3 0.000478737 0.024689 0 1.04456E‐05 0.0004787373 0.103124 0.103124 3 0.000609785 0.027864 4 0.000609785 0.027864 0 6.28835E‐05 0.000609785
160
1 0.021819 0.021819 1 0.000478729 0.0246888 2 0.000478729 0.0246888 0 1.04454E‐05 0.0004787292 0.144805 0.144805 2 0.000609785 0.027864 3 0.000609785 0.027864 0 8.82999E‐05 0.0006097853 0.042141 3 0.000609785 0.027864 4 0.000609785 0.027864 0 2.5697E‐05 0.0006097854 0.0762 0.0762 4 0.000609785 0.027864 5 0.000609785 0.027864 0 4.64656E‐05 0.0006097855 0.042141 5 0.000609785 0.027864 6 0.000609785 0.027864 0 2.5697E‐05 0.0006097856 0.0762 0.0762 6 0.000609785 0.027864 7 0.000609785 0.027864 0 4.64656E‐05 0.000609785
180 1 0.914385 0.914385 1 0.008107 0.101598 2 0.008107 0.101598 0 0.00741292 0.008107000
Test Section Parameters
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Fill/Break Component Length (m) Volume (m3) Pressure Liquid Temp
(K) Vapor Temp (K) TypeLiquid Velocity (m/s)
Vapor Velocity (m/s)
1 Fill 0.05715 1.84E‐06 1.5513E+07 550 550 Constant Velocity 0.9 0.911 Break 0.081867502 2.63E‐06 1.5513E+07 550 550 No tables 0.9 0.9
Heat Structure
Component Axial Cell Inner Surface BC Outer Surface BC
Radial Node 1 (K)
Radial Node 2 (K)
Radial Node 3 (K)
Radial Node 4 (K)
Material Region
Inner Length (m)
Outer Length (m) Material
21
1 130:1 Flux: 0.0 550 550 550 550 1 3.200E‐03 3.797E‐03 Zircaloy2 130:2 Flux: 0.0 550 550 550 550 2 3.797E‐03 3.848E‐03 Gap Gases3 130:3 Flux: 0.0 550 550 550 550 3 3.848E‐03 7.950E‐03 Mixed Oxide4 130:4 Flux: 0.0 550 550 550 5505 130:5 Flux: 0.0 550 550 550 550 Gas Gap HTC 6300 W/m2/K6 130:6 Flux: 0.0 550 550 550 5507 130:7 Flux: 0.0 550 550 550 5508 130:8 Flux: 0.0 550 550 550 5509 130:9 Flux: 0.0 550 550 550 550
10 130:10 Flux: 0.0 550 550 550 550
Power Con
nection
Component Axial Cell Relative Power Shape Radial Node Radial Locations (m)
Radial Power Shape
31
1 1 1 3.20E‐03 02 1 2 3.797E‐03 03 1 3 3.848E‐03 14 1 4 7.950E‐03 15 16 1 Power Option Constant Power7 1 Initial Power 5000 W8 19 1
10 1
Test Train Entrance Nozzle (110)
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True Geometry Calculated Geometry As-Modeled Geometry
Exit Nozzle Detail (122)
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True Geometry Calculated Geometry As-Modeled Geometry
Test Train Results
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• Steady State Calculations
• Compare to RELAP-5 simulations to determine if physics is being modeled correctly
• Change parameters to verify phenomena is being modeled as expected
Test Train Results
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0%
2%
4%
6%
8%
10%
12%
14%
570
575
580
585
590
595
600
0 5 10 15 20 25 30 35 40
Temperature
[K]
Cell
Temperature Void Frac Subcooled Boiling P = 15.5 MPaTsat = 620 K
Q = 5 kWMass flow = 0.0416 kg/s
Test Train Results
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Subcooled Boiling P = 15.5 MPaTsat = 620 K
Q = 10 kWMass flow = 0.0208 kg/s
0%
10%
20%
30%
40%
50%
60%
570
575
580
585
590
595
600
605
610
615
620
625
0 5 10 15 20 25 30 35 40
Temperature
[K]
Cell
Temperature Void Frac
Model Specific Questions
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Pipes Pump• Inner vs outer. Does it
matter?
• Appropriate power profile(axial and radial)
Heat Structure• Effective Moment of
Inertia verification
• 2-phase curves required?
• Dealing with Tee junction
• (Pipe with side junction)
• Liquid-gas interface in component 131
• Dealing with abrupt geometry changes. When to smooth out
High Level Challenges
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TRACE SNAP• Is there a manual?
• How to do axial plots? (no spatial variable to plot against)
• MATLAB Interfacing worth it? (lots of preprocessing just to organize data)
APTPlot• Model Notes?
• Improving workflow between SNAP and TRACE
• Error message explanations and causes.
• Understanding numerical instabilities.
• Access to resources beyond that of manuals.
Thank you for your time.
Questions?
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