 |
 |
 |
|
|
|
[Sponsors] | ||||
March 4, 2018, 18:30
|
ICEM Wing Mesh Problem
|
#1 |
|
New Member
Bota Amdrei
Join Date: May 2015
Posts: 13
Rep Power: 12  |
Hello everybody,
I tried to create the mesh for a wing having the aerofoil NACA23015 and my wing has round trailing edge. I cannot create the mesh at the wing tip ( see attached pictures). Thus, somehow at the walls of the domain, ICEM computed them I must say that my wing does not have a sharp trailing edge. Does someone help me with this problem ? Kind regards, Andrei Last edited by andrewmichael; March 8, 2018 at 07:15. |
|
|
|
|
 |
| Thread Tools | Search this Thread |
| Display Modes | |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| [mesh manipulation] Importing Multiple Meshes | thomasnwalshiii | OpenFOAM Meshing & Mesh Conversion | 18 | December 19, 2015 19:57 |
| [ICEM] ICEM CFD Problem with the boundary conditions while importing the mesh to fluent | sonic109 | ANSYS Meshing & Geometry | 2 | September 3, 2014 01:56 |
| Problem with usnstruct mesh Icem Tribometer | obliz | ANSYS | 0 | July 10, 2014 04:09 |
| problem when converting mesh (made by ICEM) using fluentMeshToFoam | Forrest_Lei | OpenFOAM | 11 | October 16, 2009 07:28 |
| ICEM - mesh near wing trailing edge | Joao Lourenco | CFX | 5 | August 30, 2007 18:20 |
Linear Mode
