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.
(fx66h80-il) FX 66-H-80 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Wortmann FX 66-H-80 airfoil Max thickness 8% at 27.9% chord Max camber 2.5% at 25% chord Max Cl/Cd 105.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe57-il) GOE 57 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 57 airfoil Max thickness 6.3% at 19.9% chord Max camber 5.1% at 39.9% chord Max Cl/Cd 105.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(s812-nr) NREL's S812 Airfoil | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file | |
![]() | NREL HAWT airfoil S812 primary Max thickness 21% at 39.6% chord Max camber 1.6% at 77% chord Max Cl/Cd 105.2 at Re# 1,000,000 Source NWTC National WInd Technology Center | |
(goe646-il) GOE 646 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 646 airfoil Max thickness 18.3% at 29% chord Max camber 4.5% at 49% chord Max Cl/Cd 105.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(atr72sm-il) Smoothed ATR airfoil coordinates obtained using AFSMO (Harry Morgan's NASA smoothing program) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | ATR 72 wing airfoil (from NTSB report) Max thickness 14.5% at 25.4% chord Max camber 2.9% at 21.4% chord Max Cl/Cd 105.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe796-il) GOE 796 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 796 airfoil Max thickness 12% at 30% chord Max camber 3.6% at 40% chord Max Cl/Cd 105.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(ag35-il) AG35 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Drela AG35 airfoil Max thickness 8.7% at 27.9% chord Max camber 2.3% at 37% chord Max Cl/Cd 105.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e556-il) EPPLER 556 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E556 general aviation airfoil Max thickness 16% at 31.1% chord Max camber 3.1% at 61.4% chord Max Cl/Cd 105.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(fg2-il) Fage & Collins 2 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Fage & Collins 2 airfoil Max thickness 8.2% at 30% chord Max camber 3.3% at 30% chord Max Cl/Cd 105.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe377-il) GOE 377 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 377 airfoil Max thickness 6.5% at 30% chord Max camber 3.9% at 40% chord Max Cl/Cd 105.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database |
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