Airfoil Data
E554

The EPPLER 554 AIRFOIL is a 11.5% chord-thickness airfoil with a maximum camber of 5.8% at 35% 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 E554 typically compare it against profiles of similar thickness: USA 29 AIRFOIL, NACA 64(4)-221, NACA 63(4)-221, EPPLER 396 AIRFOIL, GOE 530 AIRFOIL. The EPPLER 1233 AIRFOIL is another reference profile frequently considered alongside it.