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NACA 0012 calculation help

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06-23-15, 08:08 AM	#1
Gargamel Lucky Sailor Join Date: Oct 2010 Location: Rome Posts: 4,273 Downloads: 81 Uploads: 0	NACA 0012 calculation help Designing a new boat for an semi-open/developmental race class. Going to use a rigid sail. Planning on using a NACA0012 - NACA0015 airfoil for the wing, but I'm having trouble finding formulas for finding the surface area of a wing with a given profile, chord, and wingspan. Any aero-E's out there offer some help? __________________ Luck is a residue of Design.

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