Airfoil database search
Search the 1638 airfoils available in the databases filtering by name, thickness and camber. Click on an airfoil image to display a larger preview picture. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of Reynolds numbers.
(goe06k-il) GOE 6K AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 6K airfoil Max thickness 7.5% at 50% chord Max camber 3.1% at 50% chord Max Cl/Cd 132.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(a18sm-il) A18 (smoothed) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Archer A18 F1C free flight airfoil (smoothed) Max thickness 7.3% at 27.1% chord Max camber 3.8% at 49.3% chord Max Cl/Cd 132.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(hq309-il) HQ 3.0/9 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Quabeck HQ 3.0/9 R/C sailplane airfoil Max thickness 9% at 35% chord Max camber 3% at 50% chord Max Cl/Cd 132.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(fx66196v-il) FX 66-S-196 V1 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 66-S-196 V1 airfoil Max thickness 19.6% at 37.1% chord Max camber 4% at 46.7% chord Max Cl/Cd 132.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe692-il) GOE 692 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 692 airfoil Max thickness 16.1% at 30% chord Max camber 5% at 40% chord Max Cl/Cd 132.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(fx63137-il) WORTMANN FX 63-137 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 63-137 human power aircraft airfoil (Liver Puffin) airfoil Max thickness 13.7% at 30.9% chord Max camber 6% at 53.3% chord Max Cl/Cd 132.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(s802-nr) NREL's S802 Airfoil | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file | |
 | NREL HAWT airfoil S802 tip Not recommended Max thickness 11.5% at 37.9% chord Max camber 3.8% at 47.3% chord Max Cl/Cd 132.5 at Re# 1,000,000 Source NWTC National WInd Technology Center | |
(goe425-il) GOE 425 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 425 airfoil Max thickness 16% at 29.3% chord Max camber 4.5% at 39.3% chord Max Cl/Cd 132.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e203-il) E203 (13.64%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E203 low Reynolds number airfoil Max thickness 13.6% at 30.7% chord Max camber 2.3% at 54.1% chord Max Cl/Cd 132.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe441-il) GOE 441 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 441 airfoil Max thickness 16% at 29.5% chord Max camber 7.7% at 39.5% chord Max Cl/Cd 132.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
Please see the source web site or designer for any license conditions.