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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.

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(mh20-il) MH 20 9.01%

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MH 20  9.01%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

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FX 60-177 AIRFOILWortmann 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

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GOE 390 AIRFOILGottingen 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

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NACA 24112NACA 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

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S3021-095-84Selig 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

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HQ 3.5/18 AIRFOILQuabeck 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

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Rhode St. Genese 30Rhode 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

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NREL's S810 AirfoilNREL 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

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GOE 614 AIRFOILGottingen 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)

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USNPS4 (smoothed)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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