wrote:
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¬




Did you get the chart?


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