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.
(goe413-il) GOE 413 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 413 airfoil Max thickness 16.4% at 30% chord Max camber 4.6% at 40% chord Max Cl/Cd 52.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe320-il) GOE 320 (HANSA-BRANDENBURG II.1) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 320 (Hansa-Brandenburg II.1) airfoil Max thickness 12.3% at 29.8% chord Max camber 6.2% at 29.8% chord Max Cl/Cd 52.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(mh70-il) MH 70 11.08% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Martin Hepperle MH 70 for fying wing (full size) Max thickness 11.1% at 29.4% chord Max camber 3% at 39.6% chord Max Cl/Cd 52.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe462-il) GOE 462 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 462 airfoil Max thickness 11% at 9.9% chord Max camber 13.4% at 29.9% chord Max Cl/Cd 52.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(fx61147-il) FX 61-147 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 61-147 airfoil Max thickness 14.8% at 33.9% chord Max camber 3.2% at 33.9% chord Max Cl/Cd 52.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe286-il) GOE 286 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 286 airfoil Max thickness 9.4% at 29.9% chord Max camber 4.1% at 29.9% chord Max Cl/Cd 52.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(naca2411-il) NACA 2.5411 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA 2411 airfoil Max thickness 11% at 29.5% chord Max camber 2.5% at 39.6% chord Max Cl/Cd 52.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe675-il) GOE 675 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 675 airfoil Max thickness 14.9% at 29.5% chord Max camber 5.9% at 39.5% chord Max Cl/Cd 52.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(s4233-il) S4233-136-84 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Selig S4233 low Reynolds number airfoil Max thickness 13.6% at 34.9% chord Max camber 2.7% at 48.8% chord Max Cl/Cd 52.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe590-il) GOE 590 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 590 airfoil Max thickness 5.7% at 30% chord Max camber 4% at 30% chord Max Cl/Cd 52.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
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