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

NACA

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

Reply
 
LinkBack Thread Tools Display Modes
Old   May 18, 2001, 05:07
Default NACA
  #1
dimitris
Guest
 
Posts: n/a
Hi Suppose i have a NACA64A series airfoil lets suppose the NACA64AXYZ where XYZ are numbers does anybody can help me to find out what XYZ numbers stand for? I am interested in finding out which number of the XYZ is for the thickness which for the camber etc..

Thank u for your time in advance
  Reply With Quote

Old   May 18, 2001, 09:27
Default Re: NACA
  #2
James Date
Guest
 
Posts: n/a
Have a look in:-

Abbott and Von Doenhoeff, "Theory of Wing Sections", 1959, Dover Publications, New York.

Regards James
  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
How to import NACA 0012 Profile in Gridgen maplepink Main CFD Forum 17 May 7, 2013 13:01
Mismatched NACA profiles xTamx420 Main CFD Forum 0 July 7, 2011 10:11
Symmetric NACA Airfoil Lift and Drag Data jrider22 Main CFD Forum 3 April 15, 2010 04:59
Ansys CFX Vs. NACA Summary Report. Mismatch Result Santiago Orrego. CFX 3 February 5, 2007 13:05
NACA 0018 Airfoild in high speed flow Jason FLUENT 2 March 24, 2005 08:54


All times are GMT -4. The time now is 09:27.