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.
(goe433-il) GOE 433 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 433 airfoil Max thickness 17.4% at 29.2% chord Max camber 4.8% at 49.2% chord Max Cl/Cd 100.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe440-il) GOE 440 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 440 airfoil Max thickness 15.3% at 30% chord Max camber 9.7% at 40% chord Max Cl/Cd 100.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe116-il) GOE 116 (MVA MK.3) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 116 (MVA MK.3) airfoil Max thickness 9.3% at 39.8% chord Max camber 4.1% at 39.8% chord Max Cl/Cd 100.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(sc21006-il) NASA SC(2)-1006 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NASA SC(2)-1006 airfoil Max thickness 6% at 30% chord Max camber 2.6% at 73% chord Max Cl/Cd 100.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(geminism-il) GEMINI (smoothed) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | GEMINI R/C sailplane airfoil (smoothed) Max thickness 15.4% at 34.2% chord Max camber 2.2% at 37.9% chord Max Cl/Cd 100.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(s3002-il) SELIG 3002-099-83 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Selig S3002 low Reynolds number airfoil Max thickness 9.9% at 30.6% chord Max camber 2.3% at 49.8% chord Max Cl/Cd 100.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(mrc-20-il) MRC-20 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Drela MRC-20 Max thickness 15.6% at 38.2% chord Max camber 2.9% at 48% chord Max Cl/Cd 100.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe595-il) GOE 595 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 595 airfoil Max thickness 9.6% at 30% chord Max camber 3% at 40% chord Max Cl/Cd 100.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe612-il) GOE 612 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 612 airfoil Max thickness 15% at 29.5% chord Max camber 5% at 49.5% chord Max Cl/Cd 100 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e635-il) EPPLER 635 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E635 airfoil Max thickness 11.6% at 26.2% chord Max camber 2.9% at 22.2% chord Max Cl/Cd 100 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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