ICEM Wing Mesh Problem -- CFD Online Discussion Forums

March 4, 2018, 18:30

ICEM Wing Mesh Problem

andrewmichael

New Member

Bota Amdrei

Join Date: May 2015

Posts: 13

Rep Power: 11

andrewmichael is on a distinguished road

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

Attached Images

	2018-03-04_22h21_28.jpg (95.9 KB, 15 views)
	2018-03-04_22h19_26.jpg (171.0 KB, 13 views)
	2018-03-04_22h17_22.jpg (177.7 KB, 10 views)

Last edited by andrewmichael; March 8, 2018 at 07:15.

« Previous Thread | Next Thread »

Posting Rules
You may not post new threads You may not post replies You may not post attachments You may not edit your posts BB code is On Smilies are On [IMG] code is On HTML code is Off Trackbacks are Off Pingbacks are On Refbacks are On Forum Rules

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

All times are GMT -4. The time now is 12:43.