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.
(ah6407-il) AH-6-40-7 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Althaus AH 6-407 airfoil Max thickness 6.9% at 20% chord Max camber 5.5% at 40% chord Max Cl/Cd 121.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe376-il) GOE 376 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 376 airfoil Max thickness 6.6% at 30% chord Max camber 5% at 30% chord Max Cl/Cd 121.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe533-il) GOE 533 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 533 airfoil Max thickness 13.7% at 30% chord Max camber 4.7% at 40% chord Max Cl/Cd 121.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe517-il) GOE 517 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 517 airfoil Max thickness 7% at 30% chord Max camber 4.7% at 40% chord Max Cl/Cd 121.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e66-il) EPPLER 66 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E66 low Reynolds number airfoil Max thickness 10.1% at 28.7% chord Max camber 4.1% at 52.3% chord Max Cl/Cd 121.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe477-il) GOE 477 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 477 airfoil Max thickness 10.1% at 30% chord Max camber 4.9% at 40% chord Max Cl/Cd 121.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe612-il) GOE 612 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 612 airfoil Max thickness 15% at 29.5% chord Max camber 5% at 49.5% chord Max Cl/Cd 121.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(naca632615-il) NACA 63(2)-615 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA 63(2)-615 airfoil Max thickness 15% at 34.8% chord Max camber 3.3% at 50% chord Max Cl/Cd 121.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e209-il) E209 (13.72%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E209 low Reynolds number airfoil Max thickness 13.7% at 33.8% chord Max camber 1.6% at 48.1% chord Max Cl/Cd 121.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe407-il) GOE 407 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 407 airfoil Max thickness 9.5% at 29.9% chord Max camber 4.8% at 39.9% chord Max Cl/Cd 121.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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