Home > Forums > Software User Forums > ANSYS

2D wing in flotran

Updated Threads

Reply

Search this Thread

March 9, 2011, 08:11	2D wing in flotran	#1
stusads New Member Join Date: Mar 2011 Posts: 2 Rep Power: 0	is there a way to find the lift created by a wing using flotran in ansys 12,1? ive set up a wind tunnel scenario in 2D and i would like to know how to calculate the Coefficient of lift and coefficient of drag but i dont know how to do it. any replies would be much appreciated regards, stuart

Reply

Tags

flotran, lift coefficient, wing

« 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
3D Wing Analysis	Ed	FLUENT	5	April 13, 2019 14:07
[ICEM] O-grid around wing geometry	Anorky	ANSYS Meshing & Geometry	15	November 27, 2017 14:43
Forward swept wing simulation	abid	Siemens	1	June 16, 2012 14:26
[Gridgen] Blocking topology for blunt wing	siw	Main CFD Forum	3	July 21, 2010 14:55
Isolating wing induced drag component	siw	CFX	2	June 22, 2010 11:21

All times are GMT -4. The time now is 06:01.