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.
(hq3510-il) HQ 3.5/10 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Quabeck HQ 3.5/10 R/C sailplane airfoil Max thickness 10% at 35% chord Max camber 3.5% at 50% chord Max Cl/Cd 129.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe439-il) GOE 439 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 439 airfoil Max thickness 7.9% at 30% chord Max camber 5.2% at 40% chord Max Cl/Cd 129.3 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 129.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(usa41-il) USA 41 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | USA-41 airfoil Max thickness 6.6% at 30% chord Max camber 4.5% at 40% chord Max Cl/Cd 129.2 at Re# 1,000,000 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 129.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e639-il) EPPLER 639 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E639 airfoil Max thickness 12.6% at 29.2% chord Max camber 4.8% at 29.2% chord Max Cl/Cd 129.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe123-il) GOE 123 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 123 airfoil Max thickness 5.4% at 25% chord Max camber 5.7% at 40% chord Max Cl/Cd 129.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(s3024-il) AIRFOIL 3024 9.84% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Selig S3024 low Reynolds number airfoil Max thickness 9.8% at 30.7% chord Max camber 3% at 44.7% chord Max Cl/Cd 129 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe13k-il) GOE 13K AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 13K airfoil Max thickness 14.8% at 50% chord Max camber 5.5% at 60% chord Max Cl/Cd 129 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe225-il) GOE 225 (MVA H.35) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 225 (MVA H.35) airfoil Max thickness 12.8% at 19.7% chord Max camber 7.6% at 49.7% chord Max Cl/Cd 129 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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