aerofoil lift and drag curves (with automatic excecution) -- CFD Online Discussion Forums

February 26, 2000, 12:47	aerofoil lift and drag curves (with automatic excecution)	#1
Elizabeth Guest Posts: n/a	is it true that when doing the automatic excecution of different files, once iteration has been done and saved etc. that the lift, drag and momentum curves can not be retreived when re-reading the file case and data. Is this data inaccurate due to computational reasons or is it important and accurate? do i need these graphs and if yes can i retreave them after automatic excecution? if so how?

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
lift and drag ceofficient problem	icemaniac178	CFX	6	August 17, 2011 19:40
Lift and Drag Monitor Point Values Converging to Zero	Josh	CFX	24	May 9, 2011 11:38
Lift and Drag Forces around an Aerofoil	studentcfd	CFX	1	October 29, 2007 18:36
Correct lift but wrong pressure drag - possible?	zx	Main CFD Forum	4	July 28, 2007 00:38
Lift and Drag Coefficients Reliability	Luis	FLUENT	2	December 27, 2005 15:45

All times are GMT -4. The time now is 16:34.