Airfoil Tools
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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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(n66021-il) NACA 66-021 AIRFOIL

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NACA 66-021 AIRFOILNACA 66(4)-021 airfoil
Max thickness 21% at 45% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca0024-il) NACA 0024

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NACA 0024NACA 0024 airfoil
Max thickness 24% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(goe776-il) GOE 776 AIRFOIL

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GOE 776 AIRFOILGottingen 776 airfoil
Max thickness 25% at 30% chord
Max camber 0% at 60% chord
Source UIUC Airfoil Coordinates Database

(griffith30symsuction-il) Griffith 30% Suction Airfoil

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Griffith 30% Suction AirfoilGriffith 30% suction airfoil
Max thickness 30.6% at 49.3% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e862-il) EPPLER 862 STRUT AIRFOIL

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EPPLER 862 STRUT AIRFOILEppler E862 strut airfoil
Max thickness 32.4% at 28.5% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e863-il) EPPLER 863 STRUT AIRFOIL

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EPPLER 863 STRUT AIRFOILEppler E863 strut airfoil
Max thickness 35.7% at 28.5% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
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