Fluids

Fluids

Topics related to Fluent, CFX, Turbogrid and more.

mesh independence study for non-premixed oxy-coal combustion

    • ll00023
      Subscriber

      I am running a 2-d RANS case for non-premixed oxy-coal combustion in an elevated pressure environment.

      the models used: kw-sst for turbulence, species transport with finite rate/eddy dissipation model for combustion, DPM model for particle, DO model for radiation.

      3 meshes are generated in ICEM; quality check is good.

      the temperature, TKE, volatile concentration are quite close for these mesh. but heat of reaction profile shows big differences between coarse and medium/fine mesh.

      is this caused by finite rate/eddy dissipation model, because this model use a piece-wise function to get the reaction rate?

      Thank you.

       

       

    • Rob
      Forum Moderator

      It may also be the coarse mesh not being sufficiently resolved in the flame region. I'm assuming the particles are much smaller than the cells in all cases as you're using DPM. 

    • ll00023
      Subscriber

      Particle average size is 65 micron. they are smaller than cell size.

      I think you are right that coarse mesh is not being sufficient to resolve the flame region of the non-premixed flame at the flame front.

      the coarse mesh can capture the location of flame front, the features of turbulent flow. so now it is a cost-benefit analysis. as you can see from the table, upstream (x=0.1) temperature is similar but downstream (outlet) shows differences. I assume the downstream part does not converge well for the fine mesh.

      What's your suggestion to deal with this situation?

      Thank you for your reply, Rob. I appreciate it.

       

    • Rob
      Forum Moderator

      I'd look at contours etc to understand the flow field. A single point/surface result isn't always overly diagnostic. Why assume something when you can look at the results?

    • ll00023
      Subscriber

      The flow field looks reasonable and consistent. but I can't post it here.

      the issue here is: the inconsistence of heat of reaction at the flame front seems shaking the whole simulation's credibility.

      I assume the simulation capture the main feature of the flow and combustion. but if the goal of the simulation is to find the flame dynamics, then the mesh needs to be much finer than the current case.

    • Rob
      Forum Moderator

      And I can't comment on what I can't see. As an aside, if you're using Academic licences you do need to be publishing at some point. 

       

    • ll00023
      Subscriber

      Hi Rob, thank you for this reminder. these are the result of coarse mesh case. 

      it predicts the flame well. that's why I said the result, generally speaking, is reasonable.

       

      temp

      vel

       

    • ll00023
      Subscriber

      the data extraction location is indicated by the red line.

    • Rob
      Forum Moderator

      I checked with a colleague. As you're monitoring at a position, can you check the change in mesh hasn't move the reaction zone slightly? Also check point monitors, residuals and fluxes. 

    • ll00023
      Subscriber

      these results from coarse mesh.

      temperature at upstream. it fluctuates a little bit but I assume this is acceptable because the turbulence is expected to be strong, even if this is a RANS case.

      this is another monitor point in downstream.

      Temperature profile of three meshes: 

       

    • ll00023
      Subscriber

      mass flux shows that fine mesh case has much lower dpm mass flow rate. it is quite strange.

      in order to keep the same setting, I used file/write setting from medium mesh case and then read it to coarse and fine mesh.

       

    • Rob
      Forum Moderator

      Odd, what did you set for the injection?

    • ll00023
      Subscriber

      fine

      medium

      coarse

       

    • Rob
      Forum Moderator

      Incomplete tracks won't help. That's mass that is just "lost" in the calculation. 

    • ll00023
      Subscriber

      what's the way to reduce incomplete particle number?

      does this mean that particles are trapped in the mesh and gone?

      I increase max number of step from 5,000 to 50,000

    • ll00023
      Subscriber

      it works now.

    • Rob
      Forum Moderator

      That's better. The Max Steps meaning is covered in the various manuals: 5000 can be low for some cases.

      Incomplete means a particle runs out of integration steps and is "vanished" from the model. All mass & energy in the track is also removed from the domain. A few percent missing is fine, but with combustion you're also losing the fuel.... 

    • ll00023
      Subscriber

      it seems different meshes have different max. number of steps. if the number is too large, the simulation result is abnormal, based on the temperature profile.

    • Rob
      Forum Moderator

      That could mean you've got particles stuck somewhere. Have you plotted particle tracks along with flow field and temperature? 

    • ll00023
      Subscriber

      I didn't the diverged result due to larger max number of step. the figure below shows the particle tracks along with temperature. I didn't see any abnormal here.

    • Rob
      Forum Moderator

      Looks sensible. And the particle ages?

    • ll00023
      Subscriber

      most of particles's residual time is 3.5s. it looks reasonable

Viewing 21 reply threads
  • You must be logged in to reply to this topic.