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.
(s4083-il) S4083 (8%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Selig S4083 low Reynolds number airfoil Max thickness 8% at 22.5% chord Max camber 3.4% at 35.5% chord Max Cl/Cd 124.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe395-il) GOE 395 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 395 airfoil Max thickness 6.1% at 19.9% chord Max camber 7% at 49.9% chord Max Cl/Cd 124.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e195-il) E195 (11.82%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E195 low Reynolds number airfoil Max thickness 11.8% at 35% chord Max camber 2.7% at 44.2% chord Max Cl/Cd 124.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe424-il) GOE 424 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 424 airfoil Max thickness 19.9% at 38.5% chord Max camber 4.8% at 38.5% chord Max Cl/Cd 124.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe380-il) GOE 380 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 380 airfoil Max thickness 6.6% at 30% chord Max camber 5.6% at 30% chord Max Cl/Cd 124.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(naca644421-il) NACA 64(4)-421 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA 64(4)-421 airfoil Max thickness 20.9% at 34.8% chord Max camber 2.2% at 50% chord Max Cl/Cd 124.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(mrc-16-il) MRC-16 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Drela MRC-16 Max thickness 13.9% at 34.6% chord Max camber 3% at 40.3% chord Max Cl/Cd 124.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(fx66a175-il) WORTMANN FX 66-17A-175 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 66-17A-175 airfoil Max thickness 17.5% at 33.9% chord Max camber 4.2% at 40.2% chord Max Cl/Cd 124.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(hq258-il) HQ 2.5/8 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Quabeck HQ 2.5/8 R/C sailplane airfoil Max thickness 8% at 35% chord Max camber 2.5% at 50% chord Max Cl/Cd 124.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe399-il) GOE 399 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 399 airfoil Max thickness 6.9% at 29.9% chord Max camber 4.2% at 39.9% chord Max Cl/Cd 124.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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