How come... the fuel is still igniting at 300K?
Hello there,
I have started a couple of days ago to work on combustion simulation. i have done recently the tutorial with the liquid fuel combustion using the non-premixed model and pdf table generation. where liquid droplet of c5h12 are injected in an air stream flowing at 650K. until now everything seems ok. Next i wanted to play more with it, so i decided to change both the fuel and the air's temperature and make it 300K. In reality it can happen. no ignition should happen there... just fuel being injected... but when i ran my simulation, i ended up with a flame ! i don't know why , cane someone please explain to me what I've done wrong ... Thanks a lot |
Hey Ali, because you're not a CFD beginner, this may be a stupid question; but did you reinitialise the domain with a constant temp? Or just change the temps of the inlets?
Stu |
thanks stuarts for answering,
I didn't patch any region with a specific temperature, also temperature inlet of both fluid is 300 K. Long time no see btw, have you been on vacation ? |
Hi dimond
Basically what you are saying is not digestive as no reaction should happen at that temperature.
But still i think you should check the equation that you are using in excel or matlab . Plot k(k=k0*e6(-E/R*T) v/s T and see after what temperature the reaction starts . May be something wrong with the equation. Let me know the results. Regards shk |
Hi,
Just wondering, did you regenerate your PDF table? It may be because the PDF that is used in the simulation is still from the old temperatures. Good luck, Jenny |
Thanks guys for you answer, i made sure it's the new pdf table. both the air and the c5h12 enters at 300K. i didn't use any patch for ignition. could it be that the turbulence brought suffiant energy, or the result are wrong ?
https://dl.dropbox.com/u/35161486/how_come_1.PNG And here is the temperature profile with a maximum of 1560 K: https://dl.dropbox.com/u/35161486/how_come_2.PNG A screenshot at the droplet: https://dl.dropbox.com/u/35161486/how_come_3.PNG Thanks a lot |
Hi Ali,
One reason I can think of is that non-premixed combustion model assumes "mix is burnt", that is, reaction occurs once the fuel and oxidiser mix. That is why you don't have to patch a region of high temperature (ignition point not required). You may want to try species transport model (eg. laminar finite-rate chemistry) and compare the results with your non-premixed combustion results to see if they are the same. Good luck, Jenny |
thanks for you answes, good luck for yout oo
|
Quote:
|
My injection setting:
i'm running steady injection . Cone (droplets) with 60 degrees, and a velocity of (20 m/s) about the velocity, i don't know if it's enough. the velocity of the air where the injection starts is 10 m/s. there is also some circulation there. (the magnitude of the velocity in the tutorial is about 80) The mass flow rate is 0.00249 kg/s. i gave it 60 particles. i also set the number of tries to 10. Something i don't understand, it writes in the console that 600 injection are tracked, but 600 escaped. if they escaped, it means they didn't have the time to evaporate, so why is there a flame !!! i could have solved the problem of evaporation by reducing the diameter or increasing the max number of time step. these setting represent a mix of tutorials and my own decision as i just started. i'm not trying to replicate any experiments because simply i don't have any data. if somebody have some realistic setting applicable to combustion chamber please let me know... In general i don't understand why there is a fire at first place. Sorry for asking too much. Thanks a lot |
Just change injection angle to 30 degree (half angle should be set).
|
Quote:
that has to be applied to start angle and stop angle(air blast atomizer), where you use only half. but i think in my case the angle i gave it is really the one i see in particle plot. (from 0 degres to 90 from x axis to y axis, while the symmetry is along z) |
I really didn't understand. I have confronted with this problem before. The only problem is with your injection settings. Just change them to see their parameters effects.
|
ok i will.
|
5 Attachment(s)
Hi
I am trying to do auto ignition for nheptane/Ar/O2/N2 mixture... with adiabatic wall Can anyone suggest how to do ..ignition 1. I tried the laminer - species transport: It shows no rise in temp / pressure (I did the cold flow calculation + patch temp 1400K and species reactant), as there is no combustion even after patch temp... just increase in temperature as in attached snapshot 2. I tried the flame let model in Partially premixed but that show error in the unsteady initialisation that the mixture fraction limit is grater than the largest domain fraction even as I entered 0 in it I tried using the cold flow+ patch at 1400K the body -part in mesh , but no combustion observed , only the temp raised.... I tried then 2900K/40atm patch but no raise observed in products _ CO2 or H20 in mole fraction... In both cases the temperature just climbs to the patch value and there is no temp /pressure raise after than |
All times are GMT -4. The time now is 12:18. |