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.
(e1214-il) EPPLER 1214 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E1214 general aviation airfoil Max thickness 19.8% at 26.2% chord Max camber 2.1% at 30.4% chord Max Cl/Cd 105.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(fxs21158-il) FX S 02/1-158 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Wortmann FX S 02/1-158 airfoil Max thickness 15.8% at 30.9% chord Max camber 3.5% at 37.1% chord Max Cl/Cd 105.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(usa40-il) USA 40 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | USA-40 airfoil Max thickness 13.3% at 30% chord Max camber 4.2% at 40% chord Max Cl/Cd 105.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe384-il) GOE 384 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 384 airfoil Max thickness 19.6% at 29.3% chord Max camber 6.9% at 39.3% chord Max Cl/Cd 105.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(clarym15-il) CLARK YM-15 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | CLARK YM15 airfoil Max thickness 15% at 29.6% chord Max camber 3.6% at 39.6% chord Max Cl/Cd 105.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e328-il) EPPLER 328 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E328 flying wing airfoil Max thickness 13.3% at 31.5% chord Max camber 3% at 22.1% chord Max Cl/Cd 105.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe282-il) GOE 282 (DAIMLER XIII) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 282 (DAIMLER XIII) airfoil Max thickness 9.1% at 19.9% chord Max camber 5% at 39.9% chord Max Cl/Cd 105.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e857-il) EPPLER 857 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E857 propeller airfoil Max thickness 20.3% at 31.5% chord Max camber 4.9% at 45.1% chord Max Cl/Cd 105.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe795-il) GOE 795 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 795 airfoil Max thickness 8% at 30.9% chord Max camber 2.4% at 43.5% chord Max Cl/Cd 105 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe735-il) GOE 735 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 735 airfoil Max thickness 20.1% at 30% chord Max camber 4.4% at 30% chord Max Cl/Cd 105 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database |
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