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.
(goe796-il) GOE 796 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 796 airfoil Max thickness 12% at 30% chord Max camber 3.6% at 40% chord Max Cl/Cd 122.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(fx75193-il) WORTMANN FX 75-193 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 75-193 airfoil Max thickness 19.3% at 40.2% chord Max camber 3.7% at 69.1% chord Max Cl/Cd 122.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(s4110-il) S4110 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Selig S4110 low Reynolds number airfoil Max thickness 8.4% at 26.6% chord Max camber 3.1% at 45.4% chord Max Cl/Cd 122.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e855-il) EPPLER 855 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E855 propeller airfoil Max thickness 15.7% at 32.2% chord Max camber 3.7% at 50.6% chord Max Cl/Cd 122.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe277-il) GOE 277 (DAIMLER VIII) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 277 (DAIMLER VIII) airfoil Max thickness 8.3% at 29.9% chord Max camber 4.4% at 29.9% chord Max Cl/Cd 122.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(s4180-il) S4180-098-84 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Selig S4180 low Reynolds number airfoil Max thickness 9.8% at 26.1% chord Max camber 4% at 39.4% chord Max Cl/Cd 122.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe553-il) GOE 553 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 553 airfoil Max thickness 13.7% at 29.6% chord Max camber 4.7% at 39.6% chord Max Cl/Cd 122.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe387-il) GOE 387 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 387 airfoil Max thickness 14.9% at 30% chord Max camber 5.5% at 40% chord Max Cl/Cd 122.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe14-il) GOE 14 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 14 airfoil Max thickness 9.9% at 29.8% chord Max camber 6.9% at 29.8% chord Max Cl/Cd 122.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe182-il) GOE 182 (MVA H.27) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 182 (MVA H.27) airfoil Max thickness 9.5% at 19.9% chord Max camber 5.3% at 39.9% chord Max Cl/Cd 122.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
Please see the source web site or designer for any license conditions.