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.
(usa25-il) USA 25 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | USA-25 airfoil Max thickness 8.3% at 19.9% chord Max camber 5.2% at 29.9% chord Max Cl/Cd 124.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe423-il) GOE 423 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 423 airfoil Max thickness 16.9% at 39.7% chord Max camber 5.1% at 39.7% chord Max Cl/Cd 124.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe592-il) GOE 592 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 592 airfoil Max thickness 14.3% at 29.7% chord Max camber 7.5% at 39.7% chord Max Cl/Cd 124.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe364-il) GOE 364 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 364 airfoil Max thickness 10.8% at 30% chord Max camber 6.5% at 30% chord Max Cl/Cd 124.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e550-il) EPPLER 550 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E550 general aviation airfoil Max thickness 18.2% at 34% chord Max camber 2.2% at 29.4% chord Max Cl/Cd 124.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(raf32md-il) RAF 32 MOD AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | RAF-32 MOD airfoil Max thickness 10.2% at 30% chord Max camber 4% at 50% chord Max Cl/Cd 124.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(s4158-il) S4158 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Selig S4158 low Reynolds number airfoil Max thickness 10.9% at 35.3% chord Max camber 3.7% at 44.7% chord Max Cl/Cd 124.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(usa98-il) USA 98 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | USA-98 airfoil Max thickness 14.3% at 30% chord Max camber 6.4% at 50% chord Max Cl/Cd 124.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe167-il) GOE 167 (V.KARMAN PROP.2) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 167 (V.Karman PROP.2) airfoil Max thickness 10.1% at 29.9% chord Max camber 4.5% at 29.9% chord Max Cl/Cd 124.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(mh120-il) MH 120 11.57% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Martin Hepperle MH 120 for tip section of a propeller Max thickness 11.6% at 34.7% chord Max camber 2.2% at 44.2% chord Max Cl/Cd 124.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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