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.
(goe115-il) GOE 115 (MVA MK.2) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 115 (MVA MK.2) airfoil Max thickness 9.7% at 29.7% chord Max camber 3.7% at 39.7% chord Max Cl/Cd 102.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(m14-il) NACA M14 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA/Munk M-14 airfoil Max thickness 8.1% at 30% chord Max camber 3.9% at 30% chord Max Cl/Cd 102.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(mh117-il) MH 117 9.8% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Martin Hepperle MH 117 for a propeller for ultralight (tip) Max thickness 9.8% at 29.1% chord Max camber 2.7% at 44.6% chord Max Cl/Cd 102.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(ua2-180sm-il) UA(2)-180 smoothed | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | UA(2)-180 (smoothed) airfoil for ultralight category aircraft Max thickness 18.2% at 34.1% chord Max camber 6.5% at 39.3% chord Max Cl/Cd 102.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe417-il) GOE 417 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 417 airfoil Max thickness 6% at 20% chord Max camber 6.1% at 40% chord Max Cl/Cd 102.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe448-il) GOE 448 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 448 airfoil Max thickness 12.9% at 29.8% chord Max camber 10.5% at 39.8% chord Max Cl/Cd 102.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe269-il) GOE 269 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 269 airfoil Max thickness 6.6% at 29.9% chord Max camber 5% at 39.9% chord Max Cl/Cd 102.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(naca633618-il) NACA 63(3)-618 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA 63(3)-618 airfoil Max thickness 18% at 34.7% chord Max camber 3.3% at 50% chord Max Cl/Cd 102.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(s4083-il) S4083 (8%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Selig S4083 low Reynolds number airfoil Max thickness 8% at 22.5% chord Max camber 3.4% at 35.5% chord Max Cl/Cd 102.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe758-il) GOE 758 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 758 airfoil Max thickness 13.9% at 30% chord Max camber 4.7% at 40% chord Max Cl/Cd 102.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
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