Here is a data base of airfoils... maybe the ones you need are here.....
http://www.ae.uiuc.edu/m-selig/ads/coord_database.html
I am sure there are other data bases online if the airfoils aren't proprietary.
NACA sections are SOOOOO 20th century!! lol not frequently used these days if max performance is the goal.....
if is it possible to get X,Y,Z data points for the airfoils, then you can import this X,Y,Z data in a IBL file.....this file is a text file with the following format.....
ClosedIndexArclength
Begin section ! 1
Begin curve ! 1
118.0000000.0250000.000000
112.1000001.1003850.000000
106.2000002.8075320.000000
100.3000004.8467250.000000
you can scale the airfoil sections on the fly in the curve creation.....
the file must have an extension ".ibl" but can simply be copied and pasted into a simple text file and change the extension in windows explorer.
If you can't get X,Y,Z data, it just sucks!
email me at
mike.stroup@uav.com
as long as you don't work for northrup, I can prolly help!!!
lol