Learning Forum

[blanca.cerda]

I'm trying to inject particles for Cold Spray simulation, where I have nitrogen gas, and at the time inject the particles, this ones doesnt spread like they should. The particles should have a dispersion inside the nozzle.
am i missing something?

Any comments are appreciate,
Best regards,
Blanca

[Rob]

You're wondering why the particles don't follow the expanding flow? Why would they? 

[blanca.cerda]

Because the gas behaviour. It should look like this. 


here you have the examples, I'm testing with the configurations explained on each tesis, that i already mentioned. But doesnt look well 

[Rob]

How does the flow field look in your case? Why are the particles accelerating along the expansion nozzle and further into the plenum? Is that 2d or 2d-axi symmetric?

[blanca.cerda]

This case is 2d-axisymmetric, the particles are accelerated because the gas is accelerated through the nozzle and then they kept their momentum further. 

Here is how the flow field looks like:

[Rob]

Get rid of the size distribution and try a uniform particle size, set the injection mass for that size range. Add a few sizes (you can copy most of the injection settings). Do smaller particles follow the flow better than larger ones? Have you checked the titanium density?

[blanca.cerda]

I tried what you said, and i tried different things but happens the same. 

I am working the flow with SST k-omega, but i tried standard k-epsilon and this changed, and i got what i needed.

this is what happens with k-omega, But, even I have the same results for both for the flow, this changed with the particles, do you have if this is really something that can happen or should i consider something else if i am using sst k-omega for the particles? 

Thanks in advance

[Rob]

Why do the tracks appear to start at the entrance to the nozzle in the two more recent images?  k-e and k-w should give much the same result away from the wall, but given this is a high velocity jet I'd also consider RSM: read up on the 2-equation models and their limitations to understand why. 

[blanca.cerda]

In the last two images the injection start at the throat of the nozzle, this is something of the setup, nothing actually related or that influence this behaviour, because i also tried injecting the particle from the entrance and they have the same differences. I read both equations, but simply this doesnt make any sense. for the same configuration of fluid dinamic study and the particles, with just the difference of the turbulence model. 
In order to obtain the result i expected, i needed a Time Scale Constant for turbulent dispertion of 10 inseat of the 0.15 but i search about this and it would be ok to use 0.15 for k-omega model, and it doesnt make sense such difference between two models, because i used 0.15 of time scale for k-epsilon. The only information i got about this, is this:

it suggest to change epsilon for 0.09k/omega, in the equation 0.024 but it doesn't explain too much about the C_L. It says its not well know bot they got an aproximation that is not explained too. 

[Rob]

At the speeds you're seeing chances are there is enough compression/expansion of the flow to divert the particles. As each turbulence model will interact differently that could cause the banding. How many stochastic tries did you use?