Closed StephenCarlson closed 3 years ago
Also, the fin profile is an arbitrary airfoil shape, needs to be replaced with an actual NACA section.
Solved by ede11e9. I didn't end up adding a real airfoil shape, but I did consider the NACA 0008 or NACA 0006. The root and tip are constructed by simple bezier splines: The max thickness for the root is 6% at 27% position. The tip profile has 8% thickness at 30%.
The v1.0.x release has poor directional stability, and the tacked-on stop-gap solution with the strakes and cardboard additions should be folded into a larger set of fins which blend into what is currently the strakes.