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.
(usa29-il) USA 29 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | USA-29 airfoil Max thickness 13.2% at 29.7% chord Max camber 5.5% at 39.7% chord Max Cl/Cd 52.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(e793-il) EPPLER 793 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E793 general purpose airfoil (gyroflug speed canard canard) Max thickness 15.6% at 26.7% chord Max camber 4.2% at 44.7% chord Max Cl/Cd 52.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe566-il) GOE 566 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 566 airfoil Max thickness 8.7% at 30% chord Max camber 2.6% at 40% chord Max Cl/Cd 52.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(fx69h083-il) BELL/WORTMANN FX 69-H-083 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Bell/Wortmann FX 69-H-083 rotorcraft airfoil Max thickness 8.4% at 33.3% chord Max camber 2.5% at 33.3% chord Max Cl/Cd 52.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(e207-il) E207 (12.04%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E207 low Reynolds number airfoil Max thickness 12% at 29.6% chord Max camber 2.5% at 38.6% chord Max Cl/Cd 52.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(n63415-il) NACA 63-415 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA 63(2)-415 airfoil Max thickness 15% at 34.9% chord Max camber 2.2% at 50% chord Max Cl/Cd 52.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe298-il) GOE 298 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 298 airfoil Max thickness 12.8% at 19.6% chord Max camber 4.5% at 39.6% chord Max Cl/Cd 52.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe438-il) GOE 438 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 438 airfoil Max thickness 11% at 29.8% chord Max camber 3.8% at 39.8% chord Max Cl/Cd 52.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(usa26-il) USA 26 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | USA-26 airfoil Max thickness 9.8% at 19.9% chord Max camber 4.3% at 39.9% chord Max Cl/Cd 52.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe363-il) GOE 363 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 363 airfoil Max thickness 11.1% at 19.8% chord Max camber 5.7% at 39.8% chord Max Cl/Cd 52.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
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