|
[Sponsors] |
How can we effciently mesh for these type of geometries? |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
September 6, 2011, 01:51 |
How can we effciently mesh for these type of geometries?
|
#1 |
Senior Member
Arun raj.S
Join Date: Jul 2011
Posts: 194
Rep Power: 14 |
Hi all,
I have attached a picture of a screen geometry with this ..I want to know whats the efficient way for meshing this?...Also I want to know which type of meshing (Structured grid or Unstructured grid) I need to use .. |
|
September 6, 2011, 19:01 |
|
#2 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,703
Rep Power: 143 |
The type of mesh which is approriate also depends on the type of model you plan to do. If this is a 1mm wide liquid stirrer you would mesh it entirely differently to a 1km across wind turbine.
|
|
September 6, 2011, 23:06 |
|
#3 |
Senior Member
Arun raj.S
Join Date: Jul 2011
Posts: 194
Rep Power: 14 |
Hi I have attached the Image of geometry which I want to analyze....Have a look at it ..It is the distrtion screen which they will keep in-front of axial compressor to produce distortion
|
|
September 7, 2011, 07:51 |
|
#4 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,703
Rep Power: 143 |
You still have not answered the critical question - how big is the object, or what Re number does it run at?
Also, why are you modelling this rather than imposing its effect as a momentum sink term? |
|
September 7, 2011, 08:25 |
|
#5 |
Senior Member
Arun raj.S
Join Date: Jul 2011
Posts: 194
Rep Power: 14 |
how big is the object? 40 CM OUTER DIA AND 6 CM INNER DIA, 3 CM THICK
what Re number does it run at-- velocity -- 50 m/s reynolds n0:1235500 Also, why are you modelling this rather than imposing its effect as a momentum sink term? I don understand this question.. The main thing why am i simulating is i need to find the exit velocity components of this geometry and have to give that as entry velocity components for full rotor geometry?.. I have created the complete rotor geometry ..but i am struck with this ..I am not able to get result for this geometry..Since we don have enough computational facility we are simulating rotor and this distortion screen separately... |
|
September 7, 2011, 08:38 |
|
#6 |
Senior Member
Arun raj.S
Join Date: Jul 2011
Posts: 194
Rep Power: 14 |
I have meshed this geometries in Icem cfd with volume mesh option and then i have imported in cfx...When i run this case solver shows it has isolated volumes because of domain interface not properly designed... I DON KNOW WHAT AM I DOING WRONG...
Inlet boundary condition is Cartesian velocity components u=50 m/s v=0m/s w=om/s Outlet boundary condition is :: static pressure :: 101667 pa inteface as :: GGI inteface REMAINING FACES :: WALL :: FREE SHEAR WALL I HAVE ATTACHED THE GEOMETRY OF THE ROTOR ALSO |
|
September 7, 2011, 08:47 |
|
#7 |
Senior Member
Arun raj.S
Join Date: Jul 2011
Posts: 194
Rep Power: 14 |
i HAVE CREATED THIS SCREEN GEOMETRY IN ICEM CFD..i HAVE CREATED IT AS A PART ...i WANT TO KNOW WHETHER I HAVE TO CREATE IT AS A PART OR AN ASSEMBLY TO AVOID THESE KIND OF ISOLATED VOLUME PROBLEMS..yOUR HELP IS MUCH NEEDED HERE..
|
|
September 7, 2011, 18:56 |
|
#8 | ||
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,703
Rep Power: 143 |
Quote:
Quote:
|
|||
September 7, 2011, 23:23 |
|
#9 |
Senior Member
Arun raj.S
Join Date: Jul 2011
Posts: 194
Rep Power: 14 |
I don no how to impose its pressure drop as a momentum source term?
Could you explain in detail... Also if I wants to know if we do like that then whether we will get the exit velocity components as a file so that it will be easier for me to give it as an input for complete rotor |
|
September 8, 2011, 07:53 |
|
#10 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,703
Rep Power: 143 |
Work out a function for the drag of your body versus velocity. You should be able to do by assuming it is a cylinder and using the well known cylinder drag for this Re range. Then read the documentation about source terms and impose the drag on the flow as a momentum source term.
|
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
second order schemes | marine | OpenFOAM | 67 | April 11, 2022 18:19 |
boundary conditions for simpleFoam calculation | foam_noob | OpenFOAM Running, Solving & CFD | 8 | July 1, 2015 08:07 |
buoyantSimpleRadiationFoam | msarkar | OpenFOAM | 0 | February 15, 2010 06:22 |
[Commercial meshers] TGridFluent mesh with internal by prism layer and internal face for diagnostic | sponiar | OpenFOAM Meshing & Mesh Conversion | 2 | March 30, 2009 15:02 |
Icemcfd 11: Loss of mesh from surface mesh option? | Joe | CFX | 2 | March 26, 2007 18:10 |