Some issue with DPM
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Hi everyone,
I have some trouble with discrete phase model in fluent 15, namely no evaporated. All tracked ecaped I attached screen shot on it. mash 3500000 volumes Boundary conditions mass flow inlet 0.3 kg/s 400K pressure outlet 200000 Pa total mass fuel 0.066 kg/s (jet-a) 6 injection - Only differing localization DPM options tracking parameters - max. number of steps 100000, length scale 0.001m number of continouis phase interations per DPM iteration - 1 Spatial Discretization, first for all parametres under-relaxation factors 0.1 for all parameters First 3000 iterations is compute only cold flow and next turbulence, energy and PDF I would be grateful for any help I noticed a mistake in the first screenshot. Flow Rate it should be 0.00011 (0.0011 at present) , number of streams are correct - 10 0.00011x10 x 6(injection) gives the result the assumed 0.0066kg/s - correct me if I'm wrong |
to the best of my knowledge
no of steams=10 will not give you 10x of the mass. Instead of that go in the physical model tab, on the turbulence there and give a value of 10 there. Try it . regards shk |
Tkanks for reply,
I do not fully understand which physical model you mean. Can you explain ? regards, |
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I dont have fluent installed on my system so i cannot explain much. See in your first figure attached there. There is second tab called as physical models. In that tab there is a turbulence model parameter there. Put that value to 10 and then try, It should work reagds shk |
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go in turbulence dissipation and t ry |
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If you mean Discrete Random Walk Model I had already set 10.
The problem is located in a different place, I think. |
suchy_t
I am facing the same problem now, Did you find any solution? |
unfortunately not,
I only managed to evaporate one of the six vaporizers, bye I do not know the cause of this problem. In this moment I compute over again with different physic model. Could you write yours boundary condition? inlet outlet, kind of engine ? regards, |
i am modeling coal combustion...
i think this mass decreases because at that inlet conditions of air, it cannot properly burn the fuel. increasing velocity or temperature may help |
I still have the same problem, even if I can evaporate by changing diameter distribution to rosin-rammel the temperature in the model is not changing slightly in comparison with cold flow.
please any advice regards, |
go to
graphics and animations>> particle tracks... >> selection injection name >> summary>> track and see the report... i think you will find something |
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