Airfoil Data
E207

The E207 (12.04%) is a 8.5% chord-thickness airfoil with a maximum camber of 4.2% at 34% 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 -4.2°.

Thin airfoil theory predicts a stall angle near 11.8° and a peak lift-to-drag ratio around 59 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 E207 typically compare it against profiles of similar thickness: AH-6-40-7 AIRFOIL, GOE 394 AIRFOIL, AS6095 | Ananda-Selig | AIAA Paper 2018-0310, S1046 17% (Danny Howell), GOE 257 AIRFOIL. The GOE 498 AIRFOIL is another reference profile frequently considered alongside it.