Airfoil Data
FX63158

The FX 63-158 AIRFOIL is a 11.7% chord-thickness airfoil with a maximum camber of 5.8% at 37% 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 -5.8°.

Thin airfoil theory predicts a stall angle near 11.6° and a peak lift-to-drag ratio around 68 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 FX63158 typically compare it against profiles of similar thickness: EPPLER 580 AIRFOIL, STRAND AIRFOIL, USA 27 mod. AIRFOIL, EPPLER 582 AIRFOIL, MH 83 13.29%. The DF 101 AIRFOIL is another reference profile frequently considered alongside it.