[DesignModeler] NACA RAE 2822 Airfoil -- CFD Online Discussion Forums

December 25, 2012, 11:26

NACA RAE 2822 Airfoil

Pablo911

New Member

Paweł

Join Date: Dec 2012

Posts: 1

Rep Power: 0

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

RAE_2822_Airfoil_Coordinates01.txt (3.9 KB, 36 views)

« 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
Rae 2822	bharatiaero	Main CFD Forum	5	December 31, 2022 13:15
transonic RAE 2822 Airfoil grid..help	Michel	Main CFD Forum	6	April 14, 2019 08:45
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 00:21
Grid for RAE transonic airfoil	Michel	Main CFD Forum	0	October 11, 2002 12:16

All times are GMT -4. The time now is 18:12.