CFD Online Logo CFD Online URL
Home > Forums > ANSYS Meshing & Geometry

[DesignModeler] NACA RAE 2822 Airfoil

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

LinkBack Thread Tools Display Modes
Old   December 25, 2012, 12:26
Default NACA RAE 2822 Airfoil
New Member
Join Date: Dec 2012
Posts: 1
Rep Power: 0
Pablo911 is on a distinguished road
I am trying to create a geometry, in CFX, of an airfoil specified in the topic using coordinates in a .txt file just like in the attachment.

However, when I go to Concept/3D curve in DesignModeler and want to specify "Coordinates file" an error occurs: "Error reading coordinates file." I've been trying to do the same by Create/Point but the same error is displayed.

Does anyone know how to solve this problem?
Attached Files
File Type: txt RAE_2822_Airfoil_Coordinates01.txt (3.9 KB, 28 views)
Pablo911 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
Rae 2822 bharatiaero Main CFD Forum 4 September 25, 2011 08:16
Symmetric NACA Airfoil Lift and Drag Data jrider22 Main CFD Forum 3 April 15, 2010 04:59
Drag prediction for Naca 23012 airfoil Ravel Bogatec CFX 17 February 15, 2008 01:21
transonic RAE 2822 Airfoil Michel Main CFD Forum 5 January 17, 2003 05:13
Grid for RAE transonic airfoil Michel Main CFD Forum 0 October 11, 2002 12:16

All times are GMT -4. The time now is 14:01.