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.
(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 110.6 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 110.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(ui1720-il) UNIVERSITY OF ILLINOIS UI-1720 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | University of Illinois UI-1720 high lift airfoil Max thickness 13.8% at 19% chord Max camber 4.6% at 21.2% chord Max Cl/Cd 110.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(s8037-il) S8037 (16%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Selig S8037 low Reynolds number airfoil Max thickness 16% at 33.5% chord Max camber 1.9% at 40.4% chord Max Cl/Cd 110.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe363-il) GOE 363 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 363 airfoil Max thickness 11.1% at 19.8% chord Max camber 5.7% at 39.8% chord Max Cl/Cd 110.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e557-il) EPPLER 557 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E557 general aviation airfoil Max thickness 16% at 30.2% chord Max camber 3.7% at 60.8% chord Max Cl/Cd 110.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(s7012-il) S7012 8.75% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Selig S7012 low Reynolds number airfoil Max thickness 8.7% at 27.7% chord Max camber 1.7% at 38.1% chord Max Cl/Cd 110.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe178-il) GOE 178 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 178 airfoil Max thickness 8.5% at 30% chord Max camber 4.4% at 30% chord Max Cl/Cd 110.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe645-il) GOE 645 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 645 airfoil Max thickness 15.4% at 19.4% chord Max camber 4.8% at 39.4% chord Max Cl/Cd 110.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe374-il) GOE 374 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 374 airfoil Max thickness 6.5% at 30% chord Max camber 4.5% at 30% chord Max Cl/Cd 110.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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