Airfoil Data
STF86361

The EPPLER STF 863-615 AIRFOIL is a 11.2% chord-thickness airfoil with a maximum camber of 5.6% at 50% chord, suited to transonic and supercritical wing sections where aft-camber reduces wave drag. At zero angle of attack the cambered geometry generates positive lift, giving an estimated zero-lift angle of -5.6°.

Thin airfoil theory predicts a stall angle near 11.6° and a peak lift-to-drag ratio around 67 at typical UAV and light-aircraft Reynolds numbers — useful benchmarks before running a full XFOIL or NeuralFoil polar. The 11% thickness provides structural depth for main-spar placement without excessive drag penalty at moderate speeds.

Designers evaluating the STF86361 typically compare it against profiles of similar thickness: NACA 66(3)-418, DEFIANT CANARD BL110 AIRFOIL, EPPLER 343 AIRFOIL, GOE 29B AIRFOIL, FX 63-145 AIRFOIL. The NASA RC(5)-10 AIRFOIL is another reference profile frequently considered alongside it.