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.
(goe124-il) GOE 124 (MVA H.4) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 124 (MVA H.4) airfoil Max thickness 7.9% at 29.9% chord Max camber 5.6% at 39.9% chord Max Cl/Cd 126.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe447-il) GOE 447 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 447 airfoil Max thickness 12.7% at 29.7% chord Max camber 8% at 39.7% chord Max Cl/Cd 126.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe379-il) GOE 379 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 379 airfoil Max thickness 6.5% at 30% chord Max camber 5.2% at 40% chord Max Cl/Cd 126.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe308-il) GOE 308 (MVA H.40) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 308 (MVA H.40) airfoil Max thickness 8.1% at 29.9% chord Max camber 5% at 29.9% chord Max Cl/Cd 126.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe562-il) GOE 562 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 562 airfoil Max thickness 14.1% at 30% chord Max camber 6.3% at 30% chord Max Cl/Cd 126.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe405-il) GOE 405 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 405 airfoil Max thickness 11.1% at 30% chord Max camber 6.5% at 40% chord Max Cl/Cd 126.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe402-il) GOE 402 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 402 airfoil Max thickness 6.8% at 20% chord Max camber 5.7% at 30% chord Max Cl/Cd 126.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(m27-il) NACA M27 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA/Munk M-27 airfoil Max thickness 12% at 30.1% chord Max camber 8.4% at 30.1% chord Max Cl/Cd 126.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e433-il) EPPLER 433 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E433 sailplane airfoil Max thickness 14.2% at 42.6% chord Max camber 3.9% at 42.6% chord Max Cl/Cd 126.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(fx79w151a-il) FX 79-W-151 A | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 79-W-151 airfoil for use on wind turbines (W) A Max thickness 15.2% at 33.9% chord Max camber 3.8% at 37.1% chord Max Cl/Cd 126.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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