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Airfoil database search (NACA 6 series)

Search the 1629 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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(n63010a-il) NACA 63A010 AIRFOIL

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NACA 63A010 AIRFOILNACA 63-010A airfoil
Max thickness 10% at 35% 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

(n63015a-il) NACA 63-015A AIRFOIL

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NACA 63-015A AIRFOILNACA 63-015A airfoil
Max thickness 15% at 35% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(n63210-il) NACA 63-210 AIRFOIL

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NACA 63-210 AIRFOILNACA 63-210 airfoil
Max thickness 10% at 35% chord
Max camber 1.1% at 60% chord
Source UIUC Airfoil Coordinates Database

(n63212-il) NACA 63-212 AIRFOIL

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NACA 63-212 AIRFOILNACA 63(1)-212 airfoil
Max thickness 12% at 34.9% chord
Max camber 1.1% at 55% chord
Source UIUC Airfoil Coordinates Database

(n63215-il) NACA 63-215 AIRFOIL

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NACA 63-215 AIRFOILNACA 63(2)-215 airfoil
Max thickness 15% at 34.9% chord
Max camber 1.1% at 50% chord
Source UIUC Airfoil Coordinates Database

(n63215b-il) NACA 63(2)-215 MOD B

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NACA 63(2)-215 MOD BNACA-NASA/AMES/Hicks 63(2)-215 MOD B airfoil
Max thickness 15% at 30% chord
Max camber 1.5% at 10% chord
Source UIUC Airfoil Coordinates Database

(n63412-il) NACA 63-412 AIRFOIL

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NACA 63-412 AIRFOILNACA 63(1)-412 airfoil
Max thickness 12% at 34.9% chord
Max camber 2.2% at 50% chord
Source UIUC Airfoil Coordinates Database

(n63415-il) NACA 63-415 AIRFOIL

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NACA 63-415 AIRFOILNACA 63(2)-415 airfoil
Max thickness 15% at 34.9% chord
Max camber 2.2% at 50% chord
Source UIUC Airfoil Coordinates Database

(n64008a-il) NACA 64-008A AIRFOIL

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NACA 64-008A AIRFOILNACA 64-008A airfoil
Max thickness 8% at 40% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
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