Clark Y 20%/9% airfoil data needed.

[orla]

Hi.

I'm new at the board and I,m needing the X,Y coordinates for a Clark Y airfoil with the following dimensions.

Wingspan = 10 meters
Center chord = 2102 mm. with a Clark Y 20% thickness at 30% of chord.
Wingtip chord = 1002mm. with a Clark Y 9% thickness at 30% of chord.

The rounded wingtips will be added on the wingtip chord.

I need the information to plot in the X,Y coordinates into my CAD system, and I have had no luck using some of the free download softwares.

I hope someone can help me here and thank you in adwance.

Regards.

Orla

 

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