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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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(m3-il) NACA M3 AIRFOIL

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NACA M3 AIRFOILNACA/Munk M-3 airfoil
Max thickness 11.9% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(nacam3-il) NACA M3

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NACA M3NACA M3 airfoil
Max thickness 11.9% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(n63012a-il) NACA 63012A AIRFOIL

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NACA 63012A AIRFOILNACA 63-012A airfoil
Max thickness 12% at 35% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(n64012-il) NASA/LANGLEY 64-012 AIRFOIL

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NASA/LANGLEY 64-012 AIRFOILNACA 64(1)-012 airfoil
Max thickness 12% at 40% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx71120-il) WORTMANN FX 71-120 AIRFOIL

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WORTMANN FX 71-120 AIRFOILWortmann FX 71-120 airfoil
Max thickness 12% at 25% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca001234-il) NACA 0012-34

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NACA 0012-34NACA 0012-34 airfoil
Max thickness 12% at 40% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca001264-il) NACA 0012-64

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NACA 0012-64NACA 0012-64 airfoil
Max thickness 12% at 40% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(n64012a-il) NACA 64-012A AIRFOIL

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NACA 64-012A AIRFOILNACA 64(1)-012A airfoil
Max thickness 12% at 40% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(sc20012-il) NASA SC(2)-0012 AIRFOIL

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NASA SC(2)-0012 AIRFOILNASA SC(2)-0012 airfoil (NASA TP-2969)
Max thickness 12% at 37% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(j5012-il) J5012 12%

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J5012   12%Jef Raskin (originator of the Apple Macintosh Project) J5012 airfoil
Max thickness 12% at 34.5% chord
Max camber 0% at 83.5% chord
Source UIUC Airfoil Coordinates Database
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