CFD Online Logo CFD Online URL
Home > Forums > Main CFD Forum

Airfoil Generation & making grid over it.

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

LinkBack Thread Tools Display Modes
Old   July 17, 1999, 15:00
Default Airfoil Generation & making grid over it.
Posts: n/a
hi anybody,

I am writing a code by elliptic grid generation technique for any naca 4 series airfoils given as input. please tell me how to generate the data for any naca 4 series airfoils. thanks in advance.

have a nice week end. r.v.ramkumar July 17.
  Reply With Quote

Old   July 18, 1999, 13:27
Default Re: Airfoil Generation & making grid over it.
Posts: n/a

You can find the equation for the thickness and camber of NACA 4-digit series airfoils in the "Theory of wing sections" by Abbott and Von Deonhoff. It is not very tough to wirte a computer code for that.

Good luck, Uma
  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
swak4foam building problem GGerber OpenFOAM Installation 54 April 24, 2015 16:02
On grid independent solution for pulsatile flow David FLUENT 4 June 8, 2005 16:20
structured grid generation pertup Main CFD Forum 0 November 2, 2004 04:05
Combustion Convergence problems Art Stretton Phoenics 5 April 2, 2002 05:59
Grid Independent Solution Chuck Leakeas Main CFD Forum 2 May 26, 2000 11:18

All times are GMT -4. The time now is 20:54.