CFD Online Logo CFD Online URL
Home > Forums > Software User Forums > ANSYS

Mash for an inclined airfoil

Register Blogs Members List Search Today's Posts Mark Forums Read

LinkBack Thread Tools Display Modes
Old   June 14, 2013, 09:22
Default Mesh for an inclined airfoil
New Member
Join Date: Jun 2013
Posts: 1
Rep Power: 0
dgnd is on a distinguished road
Hello here.

I'm from france and this is my problem:

I try to simulate with ANSYS flow through airfoil NACA 0012...

It's not complicated and i successed to test for different inclinaison to get lift decrease.
I change inclinaison by component of vector for pressure, mach number on BC far-field...

But I wanna try if I can get similar result with changing inclinaison of profil, and let x-component to 1.

My problem is i can't get a right mesh: mapped face doesn't work on 1 part of my domain...

a picture to explain (mesh is not correct at down left):

Does someone have an idea why it do not working?

(I have already tried to put a inclined line to separate the circle but the result was the same)

edit: sorry for the mistake in title i tried to change for "mesh" but i can't...

Last edited by dgnd; June 14, 2013 at 10:32.
dgnd is offline   Reply With Quote


Thread Tools
Display Modes

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 On
Pingbacks are On
Refbacks are On

Similar Threads
Thread Thread Starter Forum Replies Last Post
Simulation of Axial Fan Flow using A Momentum Source Subdomain Liam CFX 28 July 16, 2013 08:24
Problem with airfoil shape optimization robyTKD SU2 Shape Design 6 June 13, 2013 19:13
Problem with restart solution in robyTKD SU2 Shape Design 21 May 29, 2013 09:26
Considering the operating point instead of the fan curve saisanthoshm88 CFX 8 August 9, 2012 06:57
Airfoil boundary condition Frank Main CFD Forum 1 April 21, 2008 18:36

All times are GMT -4. The time now is 16:32.