2D airfoil at 15deg -- CFD Online Discussion Forums

January 9, 2012, 15:28

2D airfoil at 15deg

pisanopisalo

New Member

Join Date: Jan 2012

Posts: 4

Rep Power: 14

I have tried the tutorial of a naca0012 airfoil which is done with a C-grid, and at a 6deg angle.
Here is the link to the toutorial: https://confluence.cornell.edu/displ...oil+-+Geometry

I have tried it an it works fine, but then I just changed the x and y velocitys so the airfoil is at a 15deg angle, with all the other settings the same, I run the calculation and it does not give out a result. See attached picture.

Does anyone have any idea why is this or how to correct it?
Maybe something not right in the setup?

Attached Images

Brez naslovaa.jpg (48.1 KB, 23 views)

Last edited by pisanopisalo; January 9, 2012 at 16:15.

« 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
Low Speed Airfoil	Mancusi	FLUENT	7	April 3, 2014 06:11
[GAMBIT] Meshing airfoil using .dat file problem	creggie	ANSYS Meshing & Geometry	10	June 27, 2010 19:24
Poor Residuals at Intersection Between Symmetry Plane and Airfoil Leading Edge	TWaung	CFX	2	February 16, 2010 08:11
Modeling Backflow for a 3D Airfoil (Wing of Finite Span)	Josh	CFX	9	August 18, 2009 11:31
Airfoil boundary condition	Frank	Main CFD Forum	1	April 21, 2008 18:36

All times are GMT -4. The time now is 01:07.