Home > Forums > Software User Forums > ANSYS > FLUENT

How to set the dynamic stall convergence criterion of airfoil?

Updated Threads

Reply

Search this Thread

January 10, 2013, 21:45	How to set the dynamic stall convergence criterion of airfoil?	#1
shlgzz New Member Wheeler Join Date: Jan 2013 Posts: 24 Rep Power: 13	I'm doing something about dynamic stall of airfoil ?However,I 'puzzled about the dynamic stall convergence criterion for the CL and CD changing all the time.Another question:What's dual time stepping method on transient problem? Thank U!

Reply

Tags

convergence criterion, dual time stepping method

« 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
[ICEM] ICEM Scripting Issues	tylerplowright	ANSYS Meshing & Geometry	33	September 27, 2021 16:35
Dynamic Meshing of a 2D Airfoil	fkanyako	Main CFD Forum	0	March 18, 2012 22:41
Convergence criterion	newbie	Main CFD Forum	14	November 21, 2005 00:58
Convergence criterion	Moose	Main CFD Forum	5	June 9, 2005 20:39
Looking for experiments in dynamic stall	Anton Lyaskin	Main CFD Forum	0	February 10, 2003 03:57

All times are GMT -4. The time now is 19:36.