|
[Sponsors] |
August 30, 2016, 15:35 |
Mesh generation
|
#1 |
New Member
Samraj Manickam Palvannan
Join Date: Jul 2016
Posts: 25
Rep Power: 9 |
Hello all, I have some problems generating mesh for the attached picture. Its a flow simulation model. two inlets flow into a nozzle and the flow out through outlet. The gas from 2nd inlet flows around the 1st inlet and by the exit of 1st inlet, the gas from 2nd inlet mixes and flows out. I tried meshing but the gas from 2nd inlet dont just flow around 1st but just on the top the 1st inlet walls and move to right hand side of the model. Any help or guidance on how to approach the problem would really help me a lot. Thanks very much
|
|
August 30, 2016, 15:52 |
|
#2 |
Senior Member
Filippo Maria Denaro
Join Date: Jul 2010
Posts: 6,764
Rep Power: 71 |
and why do you think that the problem is in the mesh?
|
|
August 30, 2016, 15:54 |
|
#3 |
New Member
Samraj Manickam Palvannan
Join Date: Jul 2016
Posts: 25
Rep Power: 9 |
Hallo,
Thanks for the message. Its because the fluid doesnt seem to be flowing around the first inlet. It just stops before the 1st inlet's top line. |
|
August 30, 2016, 15:56 |
|
#4 |
Senior Member
Filippo Maria Denaro
Join Date: Jul 2010
Posts: 6,764
Rep Power: 71 |
post the mesh picture around the two inlets
|
|
August 30, 2016, 23:50 |
|
#5 |
Senior Member
Michael Prinkey
Join Date: Mar 2009
Location: Pittsburgh PA
Posts: 363
Rep Power: 25 |
If you are using mass or velocity inlets, this shouldn't happen--assuming you are using an off-the-shelf CFD code. If you are using pressure inlets, flow reversal at the inlets may occur. The mass/velocity inlets define the face fluxes at the inlets to be in-bound and the flow composition will be fixed based on the BCs. For pressure inlets/outlets, the fluxes at the boundary will computed based on the defined boundary pressure value and the pressure of the cell adjacent to the boundary...that can flow in or out and the composition will be extrapolated from the adjacent cell value (and possibly the cell gradient).
|
|
August 31, 2016, 03:22 |
|
#6 |
Senior Member
Filippo Maria Denaro
Join Date: Jul 2010
Posts: 6,764
Rep Power: 71 |
I agree ... it is not possible that the mesh causes such problems ..
|
|
August 31, 2016, 06:01 |
|
#7 |
New Member
Samraj Manickam Palvannan
Join Date: Jul 2016
Posts: 25
Rep Power: 9 |
I am using velocity, density, pressure and temperature as inlet boundary conditions. Also the tool i am using is LS dyna.
|
|
August 31, 2016, 06:22 |
|
#8 |
Senior Member
Filippo Maria Denaro
Join Date: Jul 2010
Posts: 6,764
Rep Power: 71 |
||
August 31, 2016, 06:27 |
|
#9 |
New Member
Samraj Manickam Palvannan
Join Date: Jul 2016
Posts: 25
Rep Power: 9 |
Hi, i am doing mixing of two gases and combustion of gas mixture and outflow
|
|
August 31, 2016, 06:34 |
|
#10 |
New Member
Samraj Manickam Palvannan
Join Date: Jul 2016
Posts: 25
Rep Power: 9 |
yes it is compressible due to significant change in density and pressure.
|
|
August 31, 2016, 06:36 |
|
#11 |
Senior Member
Filippo Maria Denaro
Join Date: Jul 2010
Posts: 6,764
Rep Power: 71 |
compressible flow with subsonic inlet requires that one condition is from the interior. Do you satisfy that?
|
|
August 31, 2016, 06:40 |
|
#12 |
New Member
Samraj Manickam Palvannan
Join Date: Jul 2016
Posts: 25
Rep Power: 9 |
He,
I am sorry. i didnt understand you question. did you mean i should set one initial boundary condition from interior? thanks |
|
August 31, 2016, 07:01 |
|
#13 | |
Senior Member
Filippo Maria Denaro
Join Date: Jul 2010
Posts: 6,764
Rep Power: 71 |
Quote:
The opposite happens for subsonic outflow. |
||
August 31, 2016, 07:02 |
|
#14 |
New Member
Samraj Manickam Palvannan
Join Date: Jul 2016
Posts: 25
Rep Power: 9 |
okay. in this case, i give temp, velocity and density as inputs and dont set pressure value? thanks
|
|
August 31, 2016, 07:03 |
|
#15 |
Senior Member
Filippo Maria Denaro
Join Date: Jul 2010
Posts: 6,764
Rep Power: 71 |
||
August 31, 2016, 07:12 |
|
#16 |
New Member
Samraj Manickam Palvannan
Join Date: Jul 2016
Posts: 25
Rep Power: 9 |
Oh okay. Would you recómmend how i can approach this problem? i need to evaluate velocity and temperature conditions for my problem.
|
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
unstructured mesh generation with strictly constrained boundary in simple space | goujl | Mesh Generation & Pre-Processing | 0 | January 29, 2015 10:44 |
[ANSYS Meshing] Question about mesh generation learning | lnk | ANSYS Meshing & Geometry | 2 | July 7, 2012 06:45 |
ISAAC code mesh generation | morteza08 | Main CFD Forum | 0 | June 15, 2012 09:26 |
[Gmsh] 2D Mesh Generation Tutorial for GMSH | aeroslacker | OpenFOAM Meshing & Mesh Conversion | 12 | January 19, 2012 03:52 |
General questions on grid-based computing | Adrin Gharakhani | Main CFD Forum | 21 | June 5, 2000 13:47 |