Jet spray simulation, which solver we have to use
The jet is pressed through a cylindrical nozzle of a length of 70 mm and an
inner diameter of 1 mm. Afterward, it expands in initially quiescent air of atmo- spheric pressure. The jet consists of a Helium/Nitrogen mixture of a density of 0.31 kg/m3. The velocity at the nozzle outlet is approximately 200 m/s. Both the air and the jet are of a temperature of T = 293 K. How we can determine the velocity and mass fraction fields? |
You just need to use the species transport model. Other than that, nothing fancy here and just about any solver settings will work.
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confused to use solver in open foam
I appreciate your reply LuckyTran, but I'm sorry for not mentioning OpenFoam in my question. Could you please suggest a solver for that solving that situation and how can determine the velocity and mass fractions?
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Use a solver with a YEqn.H. Try reactingFOAM
The velocity is the U field and mass fraction is Y field. You don't have to do any advanced post-processing to get them. If you can setup the case properly in OpenFOAM, they are right there. |
error after replacing the components using reacting foam
I'm not sure what went wrong, can some one help....
Thanks in advance Code:
Selecting combustion model laminar<psiChemistryCombustion> |
Quick answer: Without being able to see the file "jetspray/constant/reactions", it's not possible for us to properly diagnose why this happened:
Quote:
Please follow the instructions given here, in order to make it easier for people to help you: https://www.cfd-online.com/Forums/op...-get-help.html |
5 Attachment(s)
Hi Bruno, I've corrected it but now the simulation crashed. I don't know why. Could you please suggest what changes do I need to make.
The jet is pressed through a cylindrical nozzle of a length of 70 mm and an inner diameter of 1 mm. Afterward, it expands in initially quiescent air of atmospheric pressure. The jet consists of a Helium/Nitrogen mixture of a density of 0.31 kg/m3. The velocity at the nozzle outlet is approximately 200 m/s. Both the air and the jet are of a temperature of T = 293 K. Discuss the resulting velocity and mass fraction fields. I'm trying to solve it with reactingFoam by making the chemistry off and combustion as well. but the solution is getting crashed. Attachment 67461Attachment 67456 Attachment 67457 Attachment 67458 Attachment 67460 Attachment 67461 Quote:
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Hey,
since you don't mention the error message, I assume you still have the same problem: in your thermoPhysicalProperties.txt Code:
foamChemistryThermoFile "$FOAM_CASE/constant/thermo.compressibleGas"; Code:
foamChemistryThermoFile "$FOAM_CASE/constant/thermo"; If the solver is crashing for another reason and you would like to get some help, you should consider posting at least the error message. Cheers RP |
did,, still getting error
>thanks,, I did it, still getting error as shown
Code:
virothi@COOLTEK09 MINGW64 OpenFOAM-4.x ~/react Quote:
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Quick answers:
The original error message indicated in post #5 is not clear on the origin of the problem, given that it's still listing an outdated list of chemical reactions. So it feels like there is more than one file in the "constant" folder... and this separate custom tutorial case should help divide the problems apart. |
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