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Fluids

Multiphase Eulerian-Eulerian PBM DQMOM – Setup

    • Yannik Danner
      Subscriber

      I have a question about the setup for DQMOM PBM.

      First I calculate (extern script) the six Moments for a PSD (log-normal). When i use "Load File" function in Fluent it prints out a possible inlet BC with 3 quadrature points QP0, QP1, QP2, exactly described in the Users Manual. But there are no steps described for setting BC. My expected proceding:

      Given Length value is ~equal to particle diameter

      Given volume fraction can be used to calculate inlet velocity or inlet vof

      Given m4 -> inlet m4.

      the thing i am not sure about ist how to assign these valuese to my 3 secondary phases. is -> QP0 inlet BC values for sec phase 1, QP1->sec. phase 2, QP2->sec. phase 3?

    • DrAmine
      Ansys Employee

      m4 is effective length. Once you have the information for three quadratures just provide the input (not really important what is QP0 or QP1) but afterwards after running one iteration check if the values will provide the expected PSD at domain inlet.

    • Yannik Danner
      Subscriber

      Hey, thanks for the quick feedback.

      Is there any documentation about the calculation of the Quadrature Points. Maybe there is a way to calculate them by myself or to split the PSD in my own way (to split PSD in predefined length (diameter) values)?

    • DrAmine
      Ansys Employee

      Sure there is to get them caculated by yourself. You can refer to Moment inversion of Gordon and Wheeler. You just need to know that DQMOM is a direct quadrature and that is why different to QBMM or QMOM where the moments are required. So at the end you require for every qudarature point the moment to get size and volume fraction being calculated and from that the effective length is produced. The latter as well as the volume fraction information can be used as boundary input.

    • Yannik Danner
      Subscriber

      Nice, thanks for these information.

      I am trying to simulate a bubble column via multiphase eulerian-eulerian method in combination with inhomogeneous discrete or DQMOM population balance modeling. I am using 3 secondary air phases and a primary water phase.

      Particle size range: (0.0015 -0.0095 m). For the initial BC i wanna check three dfferent superficial velocities: 2.5 mm/s, 12 mm/s and 22 mm/s. I am calculation PSD extern with log. normal distribution to split the inlet velocity to the three phases (its recommendes to use inlet vof = 0.5 for inlet BC).

      I tried to use these DQMOM-method like u said. Cases with same operation conditions worked for QMOM and without PBM (3 and 1 sec. Phases). When using DQMOM simulation runs for low superficial velocity (2.5) at inlet. When using higher superficial velocity i get very high continuity residual (4.5475e+59) and floating point exception:

       Stabilizing mp-x-momentum to enhance linear solver robustness.
              Stabilizing mp-x-momentum using GMRES to enhance linear solver robustness.
              Stabilizing mp-y-momentum to enhance linear solver robustness.
              Stabilizing mp-y-momentum using GMRES to enhance linear solver robustness.
              Stabilizing mp-z-momentum to enhance linear solver robustness.
              Stabilizing mp-z-momentum using GMRES to enhance linear solver robustness.
              Stabilizing k to enhance linear solver robustness.
              Stabilizing k using GMRES to enhance linear solver robustness.

      Divergence detected in AMG solver: k        Stabilizing vof-2 to enhance linear solver robustness.
              Stabilizing vof-2 using GMRES to enhance linear solver robustness.

      Divergence detected in AMG solver: vof-2
       turbulent viscosity limited to viscosity ratio of 1.000000e+05 in 4500 cells 

      Error at host: floating point exception

      Error at Node 0: floating point exception

      Error: floating point exception
      Error Object: #f

      Same Error while using inhomogeneous discrete method for same PSD. Is there something to consider in inlet BC spliting inlet velocity and volume fractions? I am not able to explain why discretization might be this mad for these setup when other velocitys or methods are running.

       

       

    • DrAmine
      Ansys Employee

      DQMOM might be prone to numerical issues as the quadrature is dynamically updated for every cell and sometimes the problem gets so stiff. For that reaon I highly recommend that you continue experimenting first with inhomogeneous class method. If there you still have issues then you should revisit the way you are providing the bings and the closure laws.

    • Yannik Danner
      Subscriber

       

      Thank you for your advise. I could fix the Problem by using the gas-volume-fraction instead of the inlet velocity for splitting the gas-phase in 3 secondary phases!Now the calculation is running without errors.

       

      I have another question with respect to the DQMOM inlet-BC. After using Wheeler moment-inversion ANSYS gives abscissas(diameter values) and volume fraction + m4 (both calculatet from the weights and abscissas) for the inlet BC. When using m4 values for inlet BC simulation is running without problems but the sauter diameter from secondary phase is nearly similar. With this flow profile(velocities are similar too). I expect 3 different phases with different flow profiles and sauter diameter. Absciccas here where : QP0 = 13 mm, QP2 = 10, QP3 = 8 mm. PBM options max. Length = 10mm; min. Length = 1mm; reference Length = 6.3 mm

       

      Sauter Diameter is very low in comparison with discrete and QMOM Method (6.7 ans 8 mm).

      Is it really enough to give m4 and vof values from moment inversion for inlet BC to define the different secondary phases?

       

    • DrAmine
      Ansys Employee

      From moments one can calculate the wieghts and lengths and from that the DQMOM nodes are evaluated. DQMOM is using dqmom-m4 (effective length) and the VOF of the node as BC.

    • Yannik Danner
      Subscriber

      Hey, yes thats what I expect. Caclulating weights and lengths is meaningful.

      This is my moment-inversion:

                                            QP0                           QP1                   QP2
       Length (m)                8.542875e-03        6.586689e-03        5.078440e-03
       Volume Fraction        9.340751e-02        3.345744e-01        7.201864e-02
       DQMOM-m4 (m)       7.979686e-04        2.203738e-03        3.657423e-04

      I have 3 secondary Phases (Air1, Air2, Air3).

      For BC is used: QP0 -> Air1; QP1 -> Air2 and QP2 -> Air3 (volume fraction and dqmom-m4).

      When starting Simulation I expected that the Sauter-Diameter for each phase at the inlet is:

      Air1 ~ QP0(length); Air2 ~ QP1(length); Air3 ~ QP2(length);

      But all Sauter Diameter start at 0.001 m (thats what i defined the min Size). Its not even in the NDF what i used for inlet BC.

      Why? how to define these diameter values? They are the essential values for calulating velocity.

    • DrAmine
      Ansys Employee

      You probably need to make the volume fraction input relative to the total "gas" volume fraction as stated in the Guide. Please check that on your side. For the initialization: are you using the values from Inlet. Please check that too.

       

    • Yannik Danner
      Subscriber

      "You probably need to make the volume fraction input relative to the total "gas" volume fraction as stated in the Guide."

      Thats what I do.

      "For the initialization: are you using the values from Inlet. "

      I will check that thank you.

       

      I have another question, sorry.:

      I saw that the Simulation gives Sauter mean diameter for regions with vof = 0, Sauter = 0.001 m = min. Length. Maybe thats not considered in global mean diameter and thats why its this low.

      Do Ansys calculate the Eulerian velocity based on the Sauter diameter for each cell, or based on the global sauter diameter?

       

      Sorry for dragging out this Thread but its good to have some help at this point.

       

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