Home > Forums > Software User Forums > ANSYS > FLUENT

ONERA M6 Wing Validation

Updated Threads

Reply

Search this Thread

May 27, 2024, 09:46	ONERA M6 Wing Validation	#1
JAMES_SPIR New Member Spiridakos Dimitrios Join Date: Oct 2015 Location: Athens, Greece Posts: 2 Rep Power: 0	Hi, I am trying to reproduce the ONERA M6 wing simulation in this video (https://www.youtube.com/watch?v=wnAbyAZHcGo&t=1719s), however I use ANSYS version R19.2 instead of the 2021 R1 used in the YouTube video. Although I follow every step as shown in the video, my Lift Coefficient value is 30% less than the expected. Both Pressure and Drag Coefficient are the ones expected. The simulation converged. Any ideas what could be wrong? I have done it quite a few times with the same results.

Reply

Tags

ansys 19.2, drag coefficient, lift coefficient, onera m6, validation data

« 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
Incompressible Wing Wind Tunnel Validation Data Request	cosmictrex	Main CFD Forum	0	September 30, 2021 02:28
Ffd_control_point_2d	feiyi	SU2	4	September 30, 2019 12:42
Onera M6 3D validation	cfdseeker	CFX	3	September 12, 2014 17:32
[ICEM] Onera M6 3D validation	cfdseeker	ANSYS Meshing & Geometry	0	September 12, 2014 15:09
CFX-Pre problem, pls help!!!	cth_yao	CFX	0	February 17, 2012 00:52

All times are GMT -4. The time now is 19:59.