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.
(mh20-il) MH 20 9.01% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Martin Hepperle MH 20 for F3D Pylon Racing Max thickness 9% at 32.2% chord Max camber 1.9% at 37.3% chord Max Cl/Cd 105.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(fx60177-il) FX 60-177 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Wortmann FX 60-177 airfoil Max thickness 17.7% at 37.1% chord Max camber 2.7% at 77.8% chord Max Cl/Cd 105.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe390-il) GOE 390 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 390 airfoil Max thickness 20.3% at 29.2% chord Max camber 6.9% at 39.2% chord Max Cl/Cd 105.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(naca24112-jf) NACA 24112 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file | |
![]() | NACA 24112 5 digit reflex airfoil Max thickness 12% at 29.4% chord Max camber 1.7% at 20.6% chord Max Cl/Cd 105.5 at Re# 1,000,000 Source Javafoil generated | |
(s3021-il) S3021-095-84 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Selig S3021 low Reynolds number airfoil Max thickness 9.5% at 30% chord Max camber 2.5% at 39.2% chord Max Cl/Cd 105.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(hq3518-il) HQ 3.5/18 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Quabeck HQ 3.5/18 R/C sailplane airfoil Max thickness 18% at 35% chord Max camber 3.5% at 50% chord Max Cl/Cd 105.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(rhodesg30-il) Rhode St. Genese 30 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Rhode St. Genese 30 airfoil Max thickness 9.7% at 30% chord Max camber 3.2% at 40% chord Max Cl/Cd 105.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(s810-nr) NREL's S810 Airfoil | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file | |
![]() | NREL HAWT airfoil S810 tip Max thickness 18% at 44.2% chord Max camber 0.9% at 10.9% chord Max Cl/Cd 105.4 at Re# 1,000,000 Source NWTC National WInd Technology Center | |
(goe614-il) GOE 614 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 614 airfoil Max thickness 18.8% at 29.2% chord Max camber 6.2% at 39.2% chord Max Cl/Cd 105.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(usnps4-il) USNPS4 (smoothed) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Jacobs USNPS4 (smoothed) 17.5 kW wind turbine airfoil Max thickness 11.9% at 34.2% chord Max camber 5% at 34.2% chord Max Cl/Cd 105.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database |
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