Airfoil Data
GIIII
GIII BL288 AIRFOIL
Wing Geometry Simulator
The GIII BL288 AIRFOIL is a thin 5.5% chord-thickness airfoil with a maximum camber of 2.7% at 35% chord, suited to high-speed UAVs, sailplane tip sections, and propeller blade design. At zero angle of attack the cambered geometry generates positive lift, giving an estimated zero-lift angle of -2.7°.
Thin airfoil theory predicts a stall angle near 11.9° and a peak lift-to-drag ratio around 51 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 GIIII typically compare it against profiles of similar thickness: EH 2.0/7.0, AG27 Bubble Dancer DLG by Mark Drela | The AG2x airfoils are intended to be used on composite versions of the Bubble Dancer and the Allegro-Lite., NACA/LANGLEY SYMMETRICAL, SUPERCRITICAL AIRFOIL, EH 1.0/9.0, SIKORSKY SC1095R8 AIRFOIL. The NACA 4418 is another reference profile frequently considered alongside it.
Related Airfoils
Engineers evaluating the GIIII frequently compare it against profiles with comparable geometric constraints. Below are the closest matches based on maximum thickness (5.5%) and max camber (2.7%).
EH2070
EH 2.0/7.0
DRELA-AG27
AG27 Bubble Dancer DLG by Mark Drela | The AG2x airfoils are intended to be used on composite versions of the Bubble Dancer and the Allegro-Lite.
NACA-0011SC
NACA/LANGLEY SYMMETRICAL, SUPERCRITICAL AIRFOIL
EH1090
EH 1.0/9.0
SIKORSKY-SC1095R8
SIKORSKY SC1095R8 AIRFOIL
EH2070
EH 2.0/7.0
DRELA-AG27
AG27 Bubble Dancer DLG by Mark Drela | The AG2x airfoils are intended to be used on composite versions of the Bubble Dancer and the Allegro-Lite.
NACA-0011SC
NACA/LANGLEY SYMMETRICAL, SUPERCRITICAL AIRFOIL
EH1090
EH 1.0/9.0
SIKORSKY-SC1095R8
SIKORSKY SC1095R8 AIRFOIL