CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > ANSYS > FLUENT

airfoil drag

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

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   October 28, 2002, 08:46
Default airfoil drag
  #1
aaa
Guest
 
Posts: n/a
Hi

It is difficult to caculate airfoil drag precisely,could you help me.For example,cal.NACA64a216 in Fluent S-A/K-E model,alfa=0 degree,M=0.6,the cal.result drag coefficent cd=0.035. But the real cd=0.0047.
  Reply With Quote

Old   November 6, 2002, 19:36
Default Re: airfoil drag
  #2
Amid Naz
Guest
 
Posts: n/a
are you sure about the value of (0.0047)? It seems vey low ..even (0.035)..
  Reply With Quote

Reply

Thread Tools Search this Thread
Search this Thread:

Advanced Search
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 Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
Airfoil negative drag coefficent James Forrest Main CFD Forum 9 September 5, 2022 11:30
Drag of Plunging Airfoil mahzironrazak FLUENT 0 October 19, 2009 19:41
airfoil optimizer chain with drag problem Arnolm OpenFOAM Running, Solving & CFD 2 October 18, 2009 14:43
Drag prediction for Naca 23012 airfoil Ravel Bogatec CFX 17 February 15, 2008 01:21
Airfoil Drag Force wowakai Main CFD Forum 3 October 13, 1998 20:27


All times are GMT -4. The time now is 07:38.