CFD Online Logo CFD Online URL
Home > Forums > CFX


Register Blogs Members List Search Today's Posts Mark Forums Read

LinkBack Thread Tools Display Modes
Old   June 25, 2009, 09:46
Default airfoil
New Member
ahmed nabil mahfouz
Join Date: May 2009
Posts: 6
Rep Power: 8
ahmednabil is on a distinguished road
hi, i face some problems on my work on cfx for my graduation project because i couldnt find the center of pressure or finding the moment on the airfoil around its center of pressure at (0) angle of attack because i think it calculates the torques around the global axis while i want to calculate torques around the center of pressure. i would be so grateful if you replied as soon as possible. thanks
ahmednabil is offline   Reply With Quote

Old   June 25, 2009, 18:47
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 11,295
Rep Power: 88
ghorrocks is a jewel in the roughghorrocks is a jewel in the roughghorrocks is a jewel in the rough

It is a trivial matter to transpose the global axis for torque to any axis you like. Just needs a little bit of easy physics. Look in the CFX reference manual for the available CEL expressions to help you do this.

Glenn Horrocks
ghorrocks is offline   Reply With Quote


Thread Tools
Display Modes

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 On
Pingbacks are On
Refbacks are On

Similar Threads
Thread Thread Starter Forum Replies Last Post
Low Speed Airfoil Mancusi FLUENT 7 April 3, 2014 06:11
Help needed with Cornell's Gambit airfoil tutorial AW FLUENT 6 February 26, 2010 23:42
Airfoil simulation using moving wall Alejandro NUMECA 9 November 4, 2008 03:00
Airfoil boundary condition Frank Main CFD Forum 1 April 21, 2008 18:36
Mesh geometry over airfoil with Gambit laith FLUENT 4 November 12, 2006 11:04

All times are GMT -4. The time now is 09:04.