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Airfoil database search (NACA 6 series)

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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(naca634421-il) NACA 63(4)-421

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NACA 63(4)-421NACA 63(4)-421 airfoil
Max thickness 21% at 34.8% chord
Max camber 2.2% at 50% chord
Source UIUC Airfoil Coordinates Database

(naca63a210-il) NACA 63A210

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NACA 63A210NACA 63A210 airfoil
Max thickness 10% at 34.9% chord
Max camber 1.3% at 50% chord
Source UIUC Airfoil Coordinates Database

(naca641112-il) NACA 64(1)-112

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NACA 64(1)-112NACA 64(1)-112 airfoil
Max thickness 12% at 40% chord
Max camber 0.6% at 50% chord
Source UIUC Airfoil Coordinates Database

(naca64206-il) NACA 64-206

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NACA 64-206NACA 64-206 airfoil
Max thickness 6% at 40% chord
Max camber 1.1% at 50% chord
Source UIUC Airfoil Coordinates Database

(naca64208-il) NACA 64-208

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NACA 64-208NACA 64-208 airfoil
Max thickness 8% at 40% chord
Max camber 1.1% at 50% chord
Source UIUC Airfoil Coordinates Database

(naca64209-il) NACA 64-209

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NACA 64-209NACA 64-209 airfoil
Max thickness 9% at 40% chord
Max camber 1.1% at 50% chord
Source UIUC Airfoil Coordinates Database

(naca64210-il) NACA 64-210

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NACA 64-210NACA 64-210 airfoil
Max thickness 10% at 40% chord
Max camber 1.1% at 50% chord
Source UIUC Airfoil Coordinates Database

(naca642215-il) NACA 64(2)-215

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NACA 64(2)-215NACA 64(2)-215 airfoil
Max thickness 15% at 34.9% chord
Max camber 1.1% at 50% chord
Source UIUC Airfoil Coordinates Database

(naca642415-il) NACA 64(2)-415

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NACA 64(2)-415NACA 64(2)-415 airfoil
Max thickness 15% at 34.9% chord
Max camber 2.2% at 50% chord
Source UIUC Airfoil Coordinates Database

(naca643218-il) NACA 64(3)-218

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NACA 64(3)-218NACA 64(3)-218 airfoil
Max thickness 18% at 34.9% chord
Max camber 1.1% at 50% chord
Source UIUC Airfoil Coordinates Database
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