Airfoil Data
FX72150B
WORTMANN FX 72-MS-150B AIRFOIL
Wing Geometry Simulator
The WORTMANN FX 72-MS-150B AIRFOIL is a thick 16.9% chord-thickness airfoil with a maximum camber of 8.4% at 40% chord, suited to high-lift UAV wings, RC sailplanes, and low-Reynolds-number slow-flyers. At zero angle of attack the cambered geometry generates positive lift, giving an estimated zero-lift angle of -8.4°.
Thin airfoil theory predicts a stall angle near 9.9° and a peak lift-to-drag ratio around 75 at typical UAV and light-aircraft Reynolds numbers — useful benchmarks before running a full XFOIL or NeuralFoil polar. The 17% thickness provides structural depth for main-spar placement without excessive drag penalty at moderate speeds.
Designers evaluating the FX72150B typically compare it against profiles of similar thickness: FX74_CL5_140, FX 69-274, TH 25816 HALE AIRFOIL, GOE 241 (MVA PR.1) AIRFOIL, GOE 448 AIRFOIL. The FX 72-LS-160 is another reference profile frequently considered alongside it.
Related Airfoils
Engineers evaluating the FX72150B frequently compare it against profiles with comparable geometric constraints. Below are the closest matches based on maximum thickness (16.9%) and max camber (8.4%).