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Thanks Rob for looking into this.Â
inlet-fuel is the only mass flow boundary. There is a co-flow boundary of type velocity-inlet that is defined as 1m/s in the direction normal to the boundary. There is also a larger pressure-inlet surrounding the co-flow boundary with gauge pressure set to 0 Pa (Operating pressure is 101325 Pa) The rest of the domain boundaries are pressure outlets with gauge pressure at 0 Pa.Â
Why do you think the reported mass flux through the inlet-fuel different from the one that is specified at the inlet bc panel? Would the non-reflective acoustive wave model have anything to do with this?
I first came across this issue trying to run a non-premixed model of hydrogen jet flame using compressibility effects.Â
Below is the latest flux report from my last saved dat file
The latest plot of the surface monitor: It decreases over time