The early designs of the Dyna-Foil™ fins were based on the airfoils used by the National Advisory Committee for Aeronautics (NACA) , the precursor to NASA. The codified NACA airfoils developed more than 80 years ago are the basis for most foils in use today, making them an ideal starting point.
Using powerful Computational Fluid Dynamics (CFD) calculations, Quantum was able to make several refinements to the NACA design including foil shape, thickness, aspect ratio, trailing edge profile, fairing shape and more. The final version is a foil that offers an incredible 0.78 Coefficient of Lift in reverse and 1.1 in forward in Zero Speed™ motion.
Quantum focused on one system that is capable of satisfying requirements for zero, slow, medium and higher speeds while also offering solutions for various configurations. Dyna-Foil™ can be installed with or without a pocket and maintain full functionality to up to 25 knots, while delivering lift for exceptional performance.
The Dyna-Foil™ dual-purpose, fully retractable stabilizer system delivers superior roll reduction both at Zero Speed™ and underway, while eliminating the traditional limitations of speed and performance found in conventional stabilizers.