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.
(goe738-il) GOE 738 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 738 airfoil Max thickness 15.4% at 30% chord Max camber 2.1% at 30% chord Max Cl/Cd 79.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(e542-il) EPPLER 542 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E542 general aviation airfoil Max thickness 16.9% at 41.3% chord Max camber 1.9% at 31.5% chord Max Cl/Cd 79.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(n2415-il) NACA 2415 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | NACA 2415 airfoil Max thickness 15% at 29.5% chord Max camber 2% at 39.6% chord Max Cl/Cd 79.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(ah93w215-il) AH 93-W-215 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Althaus AH 93-W-215 airfoil for use on wind turbines (W) Max thickness 21.2% at 33.9% chord Max camber 3.1% at 40.2% chord Max Cl/Cd 79.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(e221-il) E221 (9.39%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E221 low Reynolds number airfoil Max thickness 9.4% at 28.1% chord Max camber 1.6% at 32.6% chord Max Cl/Cd 79.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(e331-il) EPPLER 331 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E331 flying wing airfoil Max thickness 11.2% at 28.3% chord Max camber 2.7% at 23.6% chord Max Cl/Cd 79.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(hq1010-il) HQ 1.0/10 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Quabeck HQ 1.0/10 R/C sailplane airfoil Max thickness 10% at 35% chord Max camber 1% at 50% chord Max Cl/Cd 79.1 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(e224-il) E224 (10.17%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E224 low Reynolds number airfoil Max thickness 10.2% at 29.8% chord Max camber 1.5% at 54.2% chord Max Cl/Cd 79.1 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(s811-nr) NREL's S811 Airfoil | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file | |
![]() | NREL HAWT airfoil S811 root Max thickness 26.3% at 27.4% chord Max camber 1.7% at 76.4% chord Max Cl/Cd 79.1 at Re# 500,000 Source NWTC National WInd Technology Center | |
(ste87151-il) EPPLER STE 871-514 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler STE 871-514 airfoil Max thickness 13.9% at 47.3% chord Max camber 2.5% at 79% chord Max Cl/Cd 79.1 at Re# 500,000 Source UIUC Airfoil Coordinates Database |
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