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.
(goe584-il) GOE 584 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 584 airfoil Max thickness 12.7% at 30% chord Max camber 5% at 40% chord Max Cl/Cd 126.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(s817-nr) NREL's S817 Airfoil | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file | |
 | NREL HAWT airfoil S817 tip 16.0% Dia=30 to 50 m Re=3.0E+6 Clmax(S)=1.10 Clmax(R)=1.08 Restrained max lift coef Max thickness 16% at 51.1% chord Max camber 2.8% at 41.1% chord Max Cl/Cd 126 at Re# 1,000,000 Source NWTC National WInd Technology Center | |
(goe400-il) GOE 400 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 400 airfoil Max thickness 6.1% at 20% chord Max camber 4.9% at 40% chord Max Cl/Cd 126 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e638-il) EPPLER 638 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E638 airfoil Max thickness 12.4% at 28.5% chord Max camber 4.4% at 24.5% chord Max Cl/Cd 126 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(hq3010-il) HQ 3.0/10 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Quabeck HQ 3.0/10 R/C sailplane airfoil Max thickness 10% at 35% chord Max camber 3% at 50% chord Max Cl/Cd 126 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe323-il) GOE 323 (HANSA-BRANDENBURG V.1) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 323 (Hansa-Brandenburg V.1) airfoil Max thickness 11.1% at 29.8% chord Max camber 5.2% at 29.8% chord Max Cl/Cd 125.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe226-il) GOE 226 (MVA H.36) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 226 (MVA H.36) airfoil Max thickness 13.9% at 19.7% chord Max camber 8.1% at 49.7% chord Max Cl/Cd 125.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe174-il) GOE 174 (ALBATROS 5020) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 174 (Albatros 5020) airfoil Max thickness 8.6% at 19.9% chord Max camber 5.6% at 39.9% chord Max Cl/Cd 125.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(la2573a-il) LA2573A | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Liebeck LA2573A airfoil Max thickness 13.7% at 28.8% chord Max camber 3.2% at 26.1% chord Max Cl/Cd 125.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe336-il) GOE 336 (MVA H.44) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 336 (MVA H.44) airfoil Max thickness 9% at 29.9% chord Max camber 5.4% at 29.9% chord Max Cl/Cd 125.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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