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Airfoil database search (Symmetrical)

Search the 1636 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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(s1012-il) S1012

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S1012Selig S1012 HPV airfoil
Max thickness 12% at 37.3% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(n0012-il) NACA 0012 AIRFOILS

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NACA 0012 AIRFOILSNACA 0012 airfoil
Max thickness 12% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca16012-il) NACA 16-012

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NACA 16-012NACA 16-012 airfoil
Max thickness 12% at 50% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ea61012-il) EPPLER EA 6(-1)-012 AIRFOIL

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EPPLER EA 6(-1)-012 AIRFOILEppler EA 6(-1)-012 airfoil
Max thickness 12% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx79l120-il) FX 79-L-120

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FX 79-L-120Wortmann FX 79-L-120 symmetrical airfoil
Max thickness 12.1% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ah85l120-il) AH 85-L-120/17

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AH 85-L-120/17Althaus AH 85-L-120/17 symmetrical airfoil
Max thickness 12.1% at 43.5% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx76120-il) WORTMANN FX 76-120

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WORTMANN FX 76-120Wortmann FX 76-120 symmetrical airfoil
Max thickness 12.1% at 27.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e472-il) EPPLER 472 AIRFOIL

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EPPLER 472 AIRFOILEppler E472 aerobatic aircraft airfoil
Max thickness 12.1% at 17.5% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(lwk80120k25-il) LWK 80-120/K25

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LWK 80-120/K25LWK 80-120/K25 symmetrical airfoil
Max thickness 12.1% at 40.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca0012h-sa) NACA0012H for VAWT from Sandia report SAND80-2114

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NACA0012H for VAWT from Sandia report SAND80-2114Modified Naca 0012 airfoil for Sandia VAWT tests
Max thickness 12.2% at 22.5% chord
Max camber 0% at 0% chord
Source Sandia National Laboratories
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