CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > CFX

3D,analysis of NACA-0012,with WINGLET & non.

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

Reply
 
LinkBack Thread Tools Display Modes
Old   September 17, 2006, 03:17
Default 3D,analysis of NACA-0012,with WINGLET & non.
  #1
SAEED MAHLOO
Guest
 
Posts: n/a
I need an analysys of NACA 0012 Airfoil(chord=1 unit & SPAN =8 x chord) one time without any winglet.other time with very thin winglet(NACA 0012) installed at 90,115,125,135,145 degree ANGLE to outbord(for example the shape is for 135 deg = _____________/ & for 90 deg = _____________| ). (span of winglet is 0.5 chord of wing).upstrem velocity is 200 m/s. the output needed Cl-Cd at angle of attack between 0 to 10 degree & contour of velocity & pressure change in 3D & 2D. I need to ploting result.... PLEASE HELP ME,I have only 2 days time. PLEASE,PLEASE WITH BEST REGARDS THANK YOU

17 sep 2006

--------------------------------------------------------------------------------

  Reply With Quote

Old   September 17, 2006, 08:16
Default Re: 3D,analysis of NACA-0012,with WINGLET & non.
  #2
Joe
Guest
 
Posts: n/a
Cross posting idiots like you drive away those otherwise prepared to help.
  Reply With Quote

Old   September 17, 2006, 14:58
Default Re: 3D,analysis of NACA-0012,with WINGLET & non.
  #3
SAEED MAHLOO
Guest
 
Posts: n/a
No i have not any time I need a solved problem.!!! if you can help me please help,...... I have not any software for solving this problem. I don't how work with this software? PLEASE help me? THANK YOU
  Reply With Quote

Old   September 18, 2006, 06:00
Default Re: 3D,analysis of NACA-0012,with WINGLET & non.
  #4
Use an expert
Guest
 
Posts: n/a
Get some one else who know's what they are doing to do the work!
  Reply With Quote

Old   September 18, 2006, 17:02
Default Re: 3D,analysis of NACA-0012,with WINGLET & non.
  #5
SAEED MAHLOO
Guest
 
Posts: n/a
I did not know any expert,please say what I do?

  Reply With Quote

Old   September 22, 2006, 14:13
Default Re: 3D,analysis of NACA-0012,with WINGLET & non.
  #6
Jarmo Monttinen
Guest
 
Posts: n/a
What you are asking for cannot be done in less than 3 - 4 weeks or so, anything less than that will be done with a single mesh that does not lead to reliable results.

If you are willing to pay an expert for 3-4 weeks of work, I'm sure you can find the help you need.

Jarmo
  Reply With Quote

Reply

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
Mismatched NACA profiles xTamx420 Main CFD Forum 0 July 7, 2011 10:11
3D,analysis of NACA-0012,with WINGLET & non. SAEED MAHLOO Phoenics 4 January 9, 2009 07:34
3D,analysis of NACA-0012,with WINGLET & non. SAEED MAHLOO CD-adapco 2 September 17, 2006 14:56
3D,analysis of NACA-0012,with WINGLET & non. SAEED MAHLOO FLUENT 0 September 17, 2006 03:05
3D,analysis of NACA-0012,with WINGLET & non. SAEED MAHLOO FLUENT 0 September 17, 2006 03:04


All times are GMT -4. The time now is 15:14.