Giving you an idea of some of the forces at work (and how strong your foils have to be)
These are to be used only as general guidelines - coefficient of lift varies according to aspect ratio (and other planform factors) and Reynolds number, to name just some of the variables.
|
CL |
Description |
| 1.50 | NACA0012 at angle of attack of 15 degrees (max before it stalls) |
| 0.25 | NACA0012 at angle of attack of 3 degrees (typical leeway angle upwind) |
| 0.80 | NACA0009 at angle of attack of 10 degrees (max before it stalls) |
| 0.30 | NACA0009 at angle of attack of 3 degrees |
For maximum lift generated by your centerboard, think in terms of hullspeed upwind (if you're planing, you're probably also retracting the centerboard). For maximum lift generated by your rudder, think in terms of hgh steering angles at maximum speed downwind.
Multiply the lift generated by your centerboard by one half of its submerged length, and determine if that exceeds the righting moment that your crew can generate.