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.
(e637-il) EPPLER 637 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E637 airfoil Max thickness 12.1% at 27.6% chord Max camber 3.6% at 23.6% chord Max Cl/Cd 126.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(s826-nr) NREL's S826 Airfoil | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file | |
 | NREL HAWT airfoil S826 tip 14.0% Dia=20 to 40 m Re=1.5E+6 Clmax(S)=1.42 Clmax(R)=1.31 High max lift coef Max thickness 14% at 33.7% chord Max camber 4.3% at 62% chord Max Cl/Cd 126.7 at Re# 1,000,000 Source NWTC National WInd Technology Center | |
(sd7043-il) SD7043 (9.1%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Selig/Donovan SD7043 low Reynolds number airfoil Max thickness 9.1% at 26.6% chord Max camber 3.3% at 50.2% chord Max Cl/Cd 126.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe180-il) GOE 180 (MVA H.26) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 180 (MVA H.26) airfoil Max thickness 8.7% at 30% chord Max camber 4.4% at 40% chord Max Cl/Cd 126.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(mh112-il) MH 112 Airfoil | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Martin Hepperle MH 112 for a propeller for ultralight (root) Max thickness 16.2% at 31.8% chord Max camber 6.7% at 48.5% chord Max Cl/Cd 126.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e818-il) EPPLER 818 HYDROFOIL AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E818 hydrofoil Max thickness 9.4% at 33.1% chord Max camber 2.8% at 67% chord Max Cl/Cd 126.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe682-il) GOE 682 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 682 airfoil Max thickness 10.7% at 30% chord Max camber 4.3% at 40% chord Max Cl/Cd 126.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(sg6050-il) SG6050 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Selig / Giguere SG6050 wind turbine airfoil Max thickness 16% at 31.5% chord Max camber 3.1% at 48.9% chord Max Cl/Cd 126.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe284-il) GOE 284 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 284 airfoil Max thickness 17.7% at 29.3% chord Max camber 5.1% at 39.3% chord Max Cl/Cd 126.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe372-il) GOE 372 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 372 airfoil Max thickness 6.2% at 29.9% chord Max camber 4.3% at 39.9% chord Max Cl/Cd 126.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
Please see the source web site or designer for any license conditions.