Google Groups no longer supports new Usenet posts or subscriptions. Historical content remains viewable.
Dismiss

Help with NACA 65A007 airfoil

254 views
Skip to first unread message

Jeff W. Stewart

unread,
Jan 16, 1992, 4:56:24 PM1/16/92
to
I would like to be able to plot a NACA 65A007 (and 65A006 and 65A004)
airfoil. Can someone give me more information about this airfoil style?
Are there equations to generate its planform? Or is there a table of
(X,Y) coordidnates? Where can I find out more?

Please respond via email <j...@cc.purdue.edu>.
Thanks for any information you can provide.

- Jeff Stewart

James Sonnenmeier

unread,
Jan 17, 1992, 8:32:00 AM1/17/92
to
In article <31...@mentor.cc.purdue.edu>, j...@mentor.cc.purdue.edu (Jeff W. Stewart) writes...


try 'Theory of Wing Sections' .. I.H Abbott, A.E. Von Doenhoff

Jim

Lyman Lew

unread,
Jan 17, 1992, 1:54:18 PM1/17/92
to

All NACA airfoils that I'm aware of can be found in a book called
"Theory of Wing Sections" by Ira H. Abbott. The book is published
by Dover Publications and is a very good reference book for under
$10.00. The book will have coordinates, equations, and performance
graphs of all the NACA airfoils. Good Luck!

0 new messages