Airfoil Data
AG455CT02R

The AG455ct -02f rot. is a thin 5.0% chord-thickness airfoil with a maximum camber of 2.5% at 26% chord, suited to high-speed UAVs, sailplane tip sections, and propeller blade design. At zero angle of attack the cambered geometry generates positive lift, giving an estimated zero-lift angle of -2.5°.

Thin airfoil theory predicts a stall angle near 11.9° and a peak lift-to-drag ratio around 49 at typical UAV and light-aircraft Reynolds numbers — useful benchmarks before running a full XFOIL or NeuralFoil polar. The slim profile minimises pressure drag at higher speeds but leaves limited spar depth for structural integration.

Designers evaluating the AG455CT02R typically compare it against profiles of similar thickness: LWK 80-100, FX 79-L-100, FX 76-100, NACA M10 AIRFOIL, NACA 0010. The AG54 is another reference profile frequently considered alongside it.