Airfoil Data
GOE364

The GOE 364 AIRFOIL is a 11.9% chord-thickness airfoil with a maximum camber of 6.0% at 30% chord, suited to general-aviation and UAV wing design. At zero angle of attack the cambered geometry generates positive lift, giving an estimated zero-lift angle of -6.0°.

Thin airfoil theory predicts a stall angle near 11.6° and a peak lift-to-drag ratio around 69 at typical UAV and light-aircraft Reynolds numbers — useful benchmarks before running a full XFOIL or NeuralFoil polar. The 12% thickness provides structural depth for main-spar placement without excessive drag penalty at moderate speeds.

Designers evaluating the GOE364 typically compare it against profiles of similar thickness: Rhode St. Genese 32, AH 81-K-144 W-F KLAPPE, CLARK YH AIRFOIL, WORTMANN FX 05-188 AIRFOIL, FX 78-K-150/20. The NACA 63A010 AIRFOIL is another reference profile frequently considered alongside it.