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.
(goe366-il) GOE 366 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 366 airfoil Max thickness 13.1% at 29.8% chord Max camber 7.2% at 39.8% chord Max Cl/Cd 121.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(cootie-il) WACO COOTIE AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Waco Cootie airfoil Max thickness 8.5% at 30% chord Max camber 5.5% at 40% chord Max Cl/Cd 121.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe240-il) GOE 240 (KOLLER) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 240 (KOLLER) airfoil Max thickness 7% at 29.9% chord Max camber 5.2% at 39.9% chord Max Cl/Cd 121.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(naca652415a05-il) NACA 65(2)-415 a=0.5 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA 65(2)-415 a=0.5 airfoil Max thickness 15% at 39.9% chord Max camber 3% at 45% chord Max Cl/Cd 121.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(curtisc72-il) Curtis C-72 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Curtis C-72 airfoil Max thickness 11.7% at 30% chord Max camber 3.8% at 50% chord Max Cl/Cd 121 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe321-il) GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 321 (Hansa-Brandenburg III.1) airfoil Max thickness 11.2% at 29.9% chord Max camber 5.1% at 29.9% chord Max Cl/Cd 120.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e664-il) EPPLER 664 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E664 variable geometry sailplane airfoil Max thickness 16.6% at 45.6% chord Max camber 2.6% at 40.7% chord Max Cl/Cd 120.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe371-il) GOE 371 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 371 airfoil Max thickness 7% at 29.9% chord Max camber 4.6% at 39.9% chord Max Cl/Cd 120.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe624-il) GOE 624 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 624 airfoil Max thickness 16% at 30% chord Max camber 5.2% at 40% chord Max Cl/Cd 120.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(cr1-il) CURTISS CR-1 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Curtiss CR-1 general aviation airfoil Max thickness 12.2% at 24% chord Max camber 4.7% at 42% chord Max Cl/Cd 120.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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