High-cycle thermal fatigue in mixing Tees.
Large-Eddy simulations compared to a new
                             validation experiment
                  Johan Westin                             Pascal Veber, Lars Andersson
                  Vattenfall Research and Development AB   Onsala Ingensjörsbyrå AB
                  SE-81426 Älvkarleby, Sweden              SE-43437 Kungsbacka, Sweden
                  Carsten ‘t Mannetje                      Urban Andersson, Jan Eriksson,
                  Forsmarks Kraftgrupp AB                  Mats Henriksson
                  SE-74203 Östhammar, Sweden               Vattenfall Research and Development AB
                                                           SE-81426 Älvkarleby, Sweden
                  Farid Alavyoon                           Claes Andersson
                  Forsmarks Kraftgrupp AB                  Ringhals AB
                  SE-74203 Östhammar, Sweden               SE-43022 Väröbacka , Sweden
© Vattenfall AB
                  Outline
                  • Background
                      – Previous work by the authors
                  • New experimental validation test case (2006)
                  • Computational results (Fluent)
                      – Mesh dependence study
                      – Large Eddy Simulations (LES) compared with Detached Eddy
                        Simulations (DES)
                  • Concluding remarks
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                      Background (1)
                      Introduction
                  •    Temperature fluctuations can cause
                       thermal fatigue
                  •    Interesting case for CFD-validation
                       (unsteady flow, large fluctuation levels)
                  •    Static mixers or thermal sleeves can be
                       installed to reduce the risk for thermal
                       fatigue (but expensive)                       Static mixer (MIX-331)
                  •    Desirable with accurate predictions of the
                       risk for thermal fatigue
                  •    Structural analysis require boundary
                       conditions
                        1) Amplitudes of temperature fluctuations
                        2) Frequencies of temperature fluctuations
                        3) Heat transfer to the wall
© Vattenfall AB
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                  Background (2)
                  Previous work by the present authors
                  • Model test of a plant specific T-junction performed in 2002                                       3000 mm
                      – Geometry including upstream bends                                 D=600 mm
                                                                                                     R=1100 mm
                      – Temperature fluctuations near the wall                                     2840 mm
                        measured with thermocouples                                                                     D=200 mm
                                                                               4450 mm
                      – Several test cases (flow ratios)                                                         D2=190 mm
                                                                                                   1168 mm
                  • Computational studies                                     R=225 mm
                                                                                         1000 mm
                                                                                                                 D1=123 mm
                      –   Unsteady RANS failed to predict the temp. fluctuations
                      –   LES showed promising results
                      –   Still discrepancies (amplitude and frequencies overpredicted)
                      –   Complicated and uncertain inflow boundary conditions
                  • Need for more validation data and well-documented inflow
                    boundary conditions
© Vattenfall AB
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                  New model tests for validation of CFD (2006)
                  Test rig overview
          • Fully developed pipe flow in the cold                          • Focus on one test case
            water inlet pipe                                                      – 'T|15qC
            (>80 diameters straight section                                       – Constant flow ratio Qcold/Qhot=2
            upstream the T-junction)                                              – Equal inlet velocities in the cold
          • Pipe diameters 140 mm (cold) and                                        and hot water pipe
            100 mm (hot)
          High-level
          reservoir
                                                                                          Stagnation
                                                            >2000 (>20D)          Hot     chamber
                                                                                  water   DN300
                    Stagnation chamber
                    DN400
                                         Cold water
                                                                              z
                                                                                  x
                                            >12200 (>80D)
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                  T-junction model and measurements
                                                      T11-T12
                                                                                LDV measurements
                                      T-junction
                                      T31-T32
                                                      2D   4D   6D 8D   10D    15D          20D
                          0°
                    90°        270°
                          180°
         • Thermocouples                           • Lased Doppler Velocimetry (LDV)
           (0.13 and 0.07 mm)                        – Inlet-BCs at x/D=-3 and z/D=-3.1
                   – Located 1 mm from the             – Profiles at x/D=2.6 and 6.6
                     wall                              – Measurements at 'T|15qC and isothermal
                   – Frequency response
                                                   • Single-point Lased Induced Fluorescence (LIF)
                     30-45 Hz
                                                       – Conc. measurements at isothermal conditions
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                  Flow visualization: 50%, 100% and 200% flow
                  (Reynolds number: 0.5u105, 1.0u105 and 2.0u105)
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                  Spectra of temperature fluctuations at x=4D
                  Various flow rates
                                                   x=4D
    P vs f (Hz)
    No normalization
                                  f=4 Hz                        f=4 Hz
     P                   fD1
                    vs
   'T 2                U3
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                  Performed simulations and numerical settings
                  Influence of computational mesh                          Influence of unsteady inflow-BC
              Case        #cells   tsamp      Note        Organization     1) Vortex method
                                    (s)
                                                                           2) No perturbation
            T1vm-         0.52M    29.0    4 boundary     Forsmark
                                                                           3) Scaled isotropic turbulence
            FKA                            layer cells
                                                                                from separate input files
            T1Bvm         0.45M    21.8    no BLcells     Onsala
                                                          Vattenfall R&D
            T2vm          0.93M    19.6    More           Onsala           Comparison LES-DES
                                           uniform        Vattenfall R&D
                                                                           LES: WALE (Wall-Adaptive
            T3vm           9.5M     8.3    Similar, but   Onsala              Local Eddy viscosity model)
                                           refined                         DES: SST k-Z model
                  Numerical settings
                  •  Non-iterative time advancement (NITA): 2nd order, implicit
                  •  Pressure-velocity coupling: Fractional step
                  •  Momentum eq: Bounded central differences
                  •  Pressure: PRESTO
                  •  “Law-of-the-wall” applied near the wall (y+ typically 20-50)
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                  Instantaneous temperature fields
                    Case T2vm (0.93 Mcell)        Case T3vm (9.5 Mcell)
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                  Simulation, 9.5 Mcell
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                     Temperatures near the pipe wall
                     Different computational mesh
                  Top
Left                       Right
             Bottom
                   T  Tcold
  T*
                  Thot  Tcold
   Trms                 Trms
   'T               Thot  Tcold
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                  Velocity fluctuations at the pipe centerline
                  Different computational mesh
                    urms
                    U bulk
                       wrms
                       U bulk
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                  Velcoity spectra, pipe centreline at x=2.6D
                  Different computational mesh
                      u-component (=streamwise)        v-component (=spanwise)
                                                       (not measured)
                                                       f=4 Hz
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                  Mean velocity profiles, x/D=2.6
                  Different computational mesh
              z
                  x
        y
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                  Velocity fluctuations, x/D=2.6
                  Different computational mesh
              z
                  x
        y
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                     Mean and fluctuating temperatures
                     Comparison LES vs DES (mesh 0.93 Mcell)
Left                      Right
                    T  Tcold
    T*
                   Thot  Tcold
    Trms                 Trms
    'T               Thot  Tcold
 © Vattenfall AB
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                  Time signals
                  Comparison LES vs DES (x/D=4)
            LES
            DES
      Experiment
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                  Modelled turbulent viscosity
                  Comparison LES vs DES
                          LES                                 DES
                                Color scale: 0-0.2 kg/(ms)
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                  Concluding remarks
                  • Good agreement between simulation and model test results, also
                    with fairly coarse computational mesh
                      – Both fluctuation amplitude and spectral distribution show good
                        agreement
                      – Considerably better than in previous experiment/simulations
                      – (Indicate that the current flow case is quite ”forgiving” for LES)
                  • Insensitive to variations in the (unsteady) inlet boundary conditions
                  • However: Clear improvement of the results with a refined mesh
                      – Improved results in the entire computational domain with 9.5 Mcell
                  • Still insufficient resolution near the walls
                      – Erroneous prediction of the near-wall mean velocity profile and the
                        wall-shear stress as compared to fully developed turbulent pipe flow
                      – Detached Eddy Simulations (DES) results in better near-wall profiles,
                        but the tested model is too dissipative in order to give good predicition
                        of the temperature fluctuations
© Vattenfall AB
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                  Interested in the Vattenfall T-junction test case?
                  • The experimental data can be made available for those who are interested
                    to perform simulations
                  • In return we expect to get access to the computational results
                  • No restrictions to publish your results (reference to the source of the data)
                  • Presently computations are carried out by NRG, The Netherlands (Ed
                    Komen et al.) and ANSYS, Germany (Frank et al.)
                   If you are interested to use this test case for CFD-validation, contact
                   Johan Westin, Vattenfall Research and Development AB
                   E-mail: johan.westin@vattenfall.com
© Vattenfall AB
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