Airfoil Data
BAMBINO6
Bambino 6
Wing Geometry Simulator
The Bambino 6 is a 12.0% chord-thickness airfoil with a maximum camber of 6.0% at 40% 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 -6.0°.
Thin airfoil theory predicts a stall angle near 11.6° and a peak lift-to-drag ratio around 69 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 BAMBINO6 typically compare it against profiles of similar thickness: GOE 703 AIRFOIL, RAF 6 AIRFOIL, 12%, LE rad. 0.012, TE rad. 0.0092, NACA TR259 smoothed, NACA 0024, DAE-31 AIRFOIL, EPPLER 1214 AIRFOIL. The GOE 615 AIRFOIL is another reference profile frequently considered alongside it.
Related Airfoils
Engineers evaluating the BAMBINO6 frequently compare it against profiles with comparable geometric constraints. Below are the closest matches based on maximum thickness (12.0%) and max camber (6.0%).