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Published byDrusilla Osborne Modified over 9 years ago
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Multiphase Flow Heat Transfer in Fuel Assemblies
January 2014 ASCOMP; ASCOMP Inc. USA,
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The Westinghouse 24-rod mock-up
The Westinghouse 24-rod mock-up of SVEA-96 fuel bundle Caraghiaur & Anglart (NED, 2009)
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The Westinghouse 24-rod mock-up
The Westinghouse 24-rod mock-up of SVEA-96 fuel bundle KTH Stockholm (CFX, cells)
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The Westinghouse 24-rod mock-up
ASCOMP (TransAT, IST MESH). From CAD (left) to OST grid (right). Note that the very coarse mesh shown in right is for illustration only.
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The Westinghouse 24-rod mock-up
ASCOMP (TransAT, cells)
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The Westinghouse 24-rod mock-up
KTH Stockholm (CFX) ASCOMP (TransAT)
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The OECD PSBT 5x5 Benchmark
The OECD PSBT 5x5 Benchmark with 3 spacers (3 million cells, K-e model)
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The OECD PSBT 5x5 Benchmark
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The OECD PSBT 5x5 Benchmark
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The OECD PSBT 5x5 Benchmark
Flow field and heat contours downstream the 1st simple spacer
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The OECD PSBT 5x5 Benchmark
Flow field and heat contours downstream the 1st mixing vane
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The OECD PSBT 5x5 Benchmark
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NUPEC PWR Test Facility
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Problem Description (PSBT OECD)
P=13.0 mm Flow outlet Fuel Rod r=5 mm L=1000 mm flow cross section Heat flux q” Fig. 1. Computational domain: Dimensions & BC’s. Benchmark definition within CASL: Lakehal & Buongiorno, 2011: main changes: length reduced to 1m from 3m, power to 1.6kW from 7 MW, and thus Re=GDe/ 4.8105 to 1.0104
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Saturation temperature Saturation temperature
Problem Description (PSBT OECD) Pressure 15.5 MPa Saturation temperature 344.6C Inlet temperature 290C Mass flux 3333 kg/m2s Heat Flux 581 kW/m2 Power MW Table 1: Reference operating Cdts. for PSBT OECD cases (Rubin et al., 2010). Pressure 15.5 MPa Saturation temperature 344.6C Inlet temperature 290C Mass flux 74.1 kg/m2s (or Re=300) Heat Flux 50 kW/m2 Power 1.57 kW Table 2: Downscaled operating flow Cdts. for LES
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Flow along a heated single rod at Re*=300
Ret=300 Number of nodes Resolution Grid type total number of cells x-y z Dx+--Dy+ N blocks Grid Med 40-40 798 208 BFC 1,317,400 Grid Fine 60-60 1.600 832 6,011,200 Figure 3. Medium (left) and fine (right) grids for LES (x-y). Arrows show 00 and 450 segments q=450 q=00 SGS model: LES (Dynamic SGS model) Schemes: Central 2nd order; RK 3rd order in time Adaptive time-stepping ~ Dt = s (CFL = ) Days on the DOE Jaguar on 144 and 832 MPI // cores
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Results Figure 4. Fine vs. medium resolutions (non-scaled domain): Instantaneous cross-sectional velocities and temperature contours.
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Results Fine grid: instantaneous Fine grid: time average
Medium grid: instantaneous Medium grid: time average
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Results Fine grid: instantaneous Fine grid: time average
Medium grid: instantaneous Medium grid: time average
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Results (comparison with DNS of pipe flow)
Medium grid Fine grid Figure 7a. Mean velocity profiles across the subchannel (00 & 450) compared to the DNS of Eggels (1994). Medium grid: 0 and Fine grid: 0 & 450 Figure 7b. Time averaged normal-stresses profiles (<w’w’>)
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Global Results =1.826p/D-1.043=1.33 Quantity Medium grid Fine grid
Analytical/Exp. Pressure drop DP [Pa] 10.223 10.52 ~ 10.0 Heat transfer coefficient (HTC) at XONB [kW/m2K] 1.495 1.535 1.62 (Colburn) 2.16 (Col-W*) 1.44 (Gnielinski) 1.99 (Gnlsk-W) 1.50 (Petukov) 2.00 (Ptkov-W) Distance to XONB [m] Min-max 0.49–0.57 0.49–0.6 ~ 0.59 (Colburn) ~ 0.79 (Col-W) Thermal entry length [m] 0.21–0.28 0.21–0.29 ~ 0.29–0.46 =1.826p/D-1.043=1.33 *W means with the Weisman (1959) correction factor
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Convective boiling phenomenon: The physical reality of turbulent confined bubbly flow is way more complex than the idealized conditions considered in two-phase flow studies (smooth or sinusoidal wavy films, spherical or elliptic droplets and bubbles, etc.). Turbulence-bubbles interactions is mysterious! Bubble layer in high-subcooling, high-mass-flux, high-pressure, flow boiling of Freon near the point of DNB. The situation is qualitatively similar to the PWR hot channel during a transient overpower event.
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Bubbly-flow boiling: Debora test case (CEA)
Iso-contours of transport quantities, including liquid and vapour temperature. 2D Axisymmetric simulations TransAT.
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Bubbly-flow boiling: Debora test case (CEA)
Test Case: DEBORA Experiments of Manon et al (2000, 2001) Pipe Length: 5m Pipe Diameter: 19.2 mm
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Bubbly-flow boiling: Debora test case (CEA)
There are differences between the 2-fluid & the N-phase homogeneous models. Same grid, same turbulence model, same comp. parameters. All models fail near the wall for Tin=73.7 C Void Fraction for Case 2 & 3: Tin = 58.4 C and 63.4 C Void Fraction for Case 4 & 5: Tin = 67.9 C and C Void Fraction for Case 6 & 7: Tin = 72.6 C and 73.7 C
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Bubbly-flow boiling: Lee et al. & Tu & Yeoh (KAERI)
Test Case: Experiments of Lee, Park & Lee (2002) and Tu & Yeoh (2003) Pipe Length: 2.376m q=152.3 kW/m2 Gl=474 kg/(m2s) P=0.14 Mpa ΔTsub=11.5 K. a Norm. Radial distance Heat flux mass flux Tinlet Tsat MW/ m2 kg/m2/s K 0.1523 474 371.5 383
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Bubbly-flow boiling: Bartolomei Test Case
Test Case: Experiments of Bartolomei et al (1982) Pipe Length: 1.4m Heated Length = 1m q =1.2 MW/m2 Gl= 1500 kg/(m2s) P = 6.89 Mpa ΔTsub= 63 K.
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Heat transfer in tube buddle in a steam generator
3D Setup (SNERDI) Cold water P2=5.8MPa Tf=259 ℃ va=0.63 m/s Tsat = 271 ℃ Location and size of tube and supports Geometry of the flow field Cold water Hot Water P1=15.5MPa Ti= 322℃ vi=5.3m/s Hot water Cold water Conjugate heat transfer through the tube to heat the cold water where phase change occurs. Cross-Sectional view of support * * Coarse grid is shown to illustrate the cross-section
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Heat transfer in tube buddle in a steam generator
3D Results (SNERDI)
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NUPEC PWR Test Facility: Phase average
Testcase Pressure [MPa] Inlet Temp [°C] Power [kW] Mass Flux [kg m-2s-1] 1.2211 15 295.4 90 11 1.2223 319.6 70 1.2237 329.6 60 1.4411 10 238.9 5 1.4325 253.8 2 1.4326 268.8 Cell Size (in mm) No. of Cells No. of Processors Wall Clock Time (in days) 5.31 9216 1 0.33 2.655 73728 8 0.75 1.328 108 1.5 0.885 128 4
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NUPEC PWR Test Facility: Phase average
a) ∆x = 2.65mm b) ∆x = 1.328mm ) ∆x = 0.885mm Steady State void fraction profiles for different grids (Testcase: ).
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