SimpleFOAM: 3D NACA0012 WING -- CFD Online Discussion Forums

November 12, 2014, 19:56	SimpleFOAM: 3D NACA0012 WING	#1
Ranjan New Member Ranjan Join Date: Apr 2014 Posts: 29 Rep Power: 12	Dear Foamers I am trying to simulate flow past a NACA0012 wing. Can anyone suggest a solved case of the similar type ? I am having trouble with the boundary conditions and it seems like the Cm, Cl and Cd are off charts. The Cl is too low and the Cd is relatively higher. Thanks in advance.

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
simpleFOAM NACA0012 (α=8°) cL, cD not matching published data	jferrari	OpenFOAM Running, Solving & CFD	56	November 24, 2014 13:28
Problem with SimpleFoam for a solution around an OneraM6 wing	gara1988	OpenFOAM Running, Solving & CFD	3	November 13, 2012 05:47
simpleFoam Delta wing 3D vortex	rafamusura	OpenFOAM Running, Solving & CFD	2	April 9, 2012 23:53
Naca0012 k-e mpirun gives fpe whereas simpleFoam not	Pierpaolo	OpenFOAM	1	May 8, 2010 03:08
Stalling problem with simpleFoam on a NACA0012	Damien	OpenFOAM Running, Solving & CFD	1	March 3, 2010 07:46

All times are GMT -4. The time now is 22:29.