Thank you all very much for the info. Your comments are very helpful!

Bart

On Mar 27, 9:25 am, Philippe Vessaire wrote:
wrote:
I need some information about Clark Y profiles. I found a lot of
information like coordinates, but I really need design parameters.
Like design lift coefficient, nose radius and trailing edge radius.
I would really appreciate your help!

Google : "airfoil data"
next
Google : Xfoil

and you will be happy.

--
Volem rien foutre al païs!
Philippe Vessaire Ò¿Ó¬