|
[Sponsors] |
May 29, 2020, 11:38 |
How to: RAE 2822 2D mesh from SU2
|
#1 |
Member
Zeno
Join Date: Sep 2013
Location: Delft, The Netherlands
Posts: 63
Rep Power: 13 |
Hi all,
Do you know how to obtain the mesh in the first two images below? I have downloaded it from SU2's github repository and I would like to learn how to build it from scratch. Somehow, I have managed to build the structured part of the mesh, but I cannot replicate the unstructured part. 1.jpg 2.jpg As 'Solve' parameters, I am using the Advancing Front as algorithm and a boundary decay of 0.99 but this creates the mesh below. 3.jpg Any help is appreciated, Thanks. Z |
|
August 22, 2020, 14:56 |
|
#2 |
Senior Member
Tom-Robin Teschner
Join Date: Dec 2011
Location: Cranfield, UK
Posts: 211
Rep Power: 17 |
Looks like a fairly straight forward application of the Delaunay algorithm. Try that instead and you should see something similar.
Edit: Just realised that this thread is quite old (that issues has probably been fixed). |
|
Tags |
hybrid grid, rae2822, supercritical airfoil |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
sliding mesh problem in CFX | Saima | CFX | 46 | September 11, 2021 08:38 |
GeometricField -> mesh() Function | Tobi | OpenFOAM Programming & Development | 10 | November 19, 2020 12:33 |
Salome cgns format mesh to SU2 | JPBLourenco | SU2 | 19 | November 18, 2019 03:11 |
Star CCM Overset Mesh Error (Rotating Turbine) | thezack | Siemens | 7 | October 12, 2016 12:14 |
[snappyHexMesh] snappyHexMesh won't work - zeros everywhere! | sc298 | OpenFOAM Meshing & Mesh Conversion | 2 | March 27, 2011 22:11 |