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Airfoil database list (N).

NACA 2410 to NACA 63(3)-218

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(naca2410-il) NACA 2410

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NACA 2410NACA 2410 airfoil
Max thickness 10% at 29.9% chord
Max camber 2% at 40% chord
Source UIUC Airfoil Coordinates Database

(naca2411-il) NACA 2.5411

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NACA 2.5411NACA 2411 airfoil
Max thickness 11% at 29.5% chord
Max camber 2.5% at 39.6% chord
Source UIUC Airfoil Coordinates Database

(naca24112-jf) NACA 24112

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NACA 24112NACA 24112 5 digit reflex airfoil
Max thickness 12% at 29.4% chord
Max camber 1.7% at 20.6% chord
Source Javafoil generated

(naca2412-il) NACA 2412

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NACA 2412NACA 2412 airfoil
Max thickness 12% at 30% chord
Max camber 2% at 40% chord
Source UIUC Airfoil Coordinates Database

(naca2415-il) NACA 2415

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NACA 2415NACA 2415 airfoil
Max thickness 15% at 30% chord
Max camber 2% at 40% chord
Source UIUC Airfoil Coordinates Database

(naca2418-il) NACA 2418

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NACA 2418NACA 2418 airfoil
Max thickness 18% at 30% chord
Max camber 2% at 40% chord
Source UIUC Airfoil Coordinates Database

(naca2421-il) NACA 2421

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NACA 2421NACA 2421 airfoil
Max thickness 21% at 30% chord
Max camber 2% at 40% chord
Source UIUC Airfoil Coordinates Database

(naca2424-il) NACA 2424

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NACA 2424NACA 2424 airfoil
Max thickness 24% at 29.7% chord
Max camber 2% at 40% chord
Source UIUC Airfoil Coordinates Database

(naca25112-jf) NACA 25112

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NACA 25112NACA 25112 5 digit reflex airfoil
Max thickness 12% at 29.5% chord
Max camber 2% at 27.2% chord
Source Javafoil generated

(naca4412-il) NACA 4412

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NACA 4412NACA 4412 airfoil
Max thickness 12% at 30% chord
Max camber 4% at 40% chord
Source UIUC Airfoil Coordinates Database

(naca4415-il) NACA 4415

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NACA 4415NACA 4415 airfoil
Max thickness 15% at 30.9% chord
Max camber 4% at 40.2% chord
Source UIUC Airfoil Coordinates Database

(naca4418-il) NACA 4418

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NACA 4418NACA 4418 airfoil
Max thickness 18% at 30% chord
Max camber 4% at 40% chord
Source UIUC Airfoil Coordinates Database

(naca4421-il) NACA 4421

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NACA 4421NACA 4421 airfoil
Max thickness 21% at 30% chord
Max camber 4% at 40% chord
Source UIUC Airfoil Coordinates Database

(naca4424-il) NACA 4424

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NACA 4424NACA 4424 airfoil
Max thickness 24% at 29.4% chord
Max camber 4% at 40% chord
Source UIUC Airfoil Coordinates Database

(naca63206-il) NACA 63-206

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NACA 63-206NACA 63-206 airfoil
Max thickness 6% at 35% chord
Max camber 1.1% at 50% chord
Source UIUC Airfoil Coordinates Database

(naca63209-il) NACA 63-209

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NACA 63-209NACA 63-209 airfoil
Max thickness 9% at 35% chord
Max camber 1.1% at 50% chord
Source UIUC Airfoil Coordinates Database

(naca632615-il) NACA 63(2)-615

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NACA 63(2)-615NACA 63(2)-615 airfoil
Max thickness 15% at 34.8% chord
Max camber 3.3% at 50% chord
Source UIUC Airfoil Coordinates Database

(naca632a015-il) NACA 63(2)A-015

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NACA 63(2)A-015NACA 63(2)A-015 airfoil
Max thickness 15% at 37.1% chord
Max camber 1.7% at 14.6% chord
Source UIUC Airfoil Coordinates Database

(naca633018-il) NACA 63(3)-018

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NACA 63(3)-018NACA 63(3)-018 airfoil
Max thickness 18% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca633218-il) NACA 63(3)-218

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NACA 63(3)-218NACA 63(3)-218 airfoil
Max thickness 18% at 34.9% chord
Max camber 1.1% at 24.9% chord
Source UIUC Airfoil Coordinates Database
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