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-   -   NACA 0012 calculation help (https://www.subsim.com/radioroom/showthread.php?t=220783)

Gargamel 06-23-15 08:08 AM

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?


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