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Airfoil database list (N).

NACA-0009 9.0% Smoothed to NACA 63012A AIRFOIL

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(n0009sm-il) NACA-0009 9.0% smoothed

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NACA-0009 9.0% smoothedNACA 0009 airfoil (smoothed)
Max thickness 9% at 30.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(n0011sc-il) NACA/LANGLEY SYMMETRICAL

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NACA/LANGLEY SYMMETRICALNASA/Langley 11% symmetrical supercritical airfoil
Max thickness 11% at 40% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(n0012-il) NACA 0012 AIRFOILS

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NACA 0012 AIRFOILSNACA 0012 airfoil
Max thickness 12% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(n10-il) N-10

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N-10N-10 airfoil
Max thickness 11.2% at 30% chord
Max camber 3.6% at 40% chord
Source UIUC Airfoil Coordinates Database

(n11-il) N-11

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N-11N-11 airfoil
Max thickness 10.9% at 30% chord
Max camber 4.4% at 40% chord
Source UIUC Airfoil Coordinates Database

(n11h9-il) NACA 11-H-09 AIRFOIL

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NACA 11-H-09 AIRFOILNACA 11-H-9 rotorcraft airfoil
Max thickness 9% at 40.2% chord
Max camber 4.5% at 30% chord
Source UIUC Airfoil Coordinates Database

(n12-il) N-12

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N-12N-12 airfoil
Max thickness 10.5% at 30% chord
Max camber 0.2% at 15% chord
Source UIUC Airfoil Coordinates Database

(n13-il) N-13

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N-13N-13 airfoil
Max thickness 11.8% at 30% chord
Max camber 0.1% at 95% chord
Source UIUC Airfoil Coordinates Database

(n14-il) N-14

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N-14N-14 airfoil
Max thickness 11.5% at 30% chord
Max camber 0.1% at 20% chord
Source UIUC Airfoil Coordinates Database

(n1h15-il) NACA 1-H-15 AIRFOIL

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NACA 1-H-15 AIRFOILNACA 1-H-15 rotorcraft airfoil
Max thickness 14.7% at 40% chord
Max camber 5.5% at 40% chord
Source UIUC Airfoil Coordinates Database

(n22-il) N-22

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N-22N-22 airfoil
Max thickness 12.4% at 30% chord
Max camber 4% at 40% chord
Source UIUC Airfoil Coordinates Database

(n24-il) N-24

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N-24N-24 airfoil
Max thickness 17% at 30% chord
Max camber 5.4% at 40% chord
Source UIUC Airfoil Coordinates Database

(n2414-il) NACA 2414

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NACA 2414NACA 2414 airfoil
Max thickness 14% at 29.5% chord
Max camber 2% at 39.6% chord
Source UIUC Airfoil Coordinates Database

(n2415-il) NACA 2415

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NACA 2415NACA 2415 airfoil
Max thickness 15% at 29.5% chord
Max camber 2% at 39.6% chord
Source UIUC Airfoil Coordinates Database

(n2h15-il) NACA 2-H-15 AIRFOIL

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NACA 2-H-15 AIRFOILNACA 2-H-15 rotorcraft airfoil
Max thickness 14.7% at 40% chord
Max camber 4.5% at 40% chord
Source UIUC Airfoil Coordinates Database

(n5h10-il) NACA 5-H-10 AIRFOIL

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NACA 5-H-10 AIRFOILNACA 5-H-10 rotorcraft airfoil
Max thickness 9.9% at 40% chord
Max camber 2.3% at 40% chord
Source UIUC Airfoil Coordinates Database

(n5h15-il) NACA 5-H-15 AIRFOIL

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NACA 5-H-15 AIRFOILNACA 5-H-15 rotorcraft airfoil
Max thickness 15.4% at 40% chord
Max camber 2.9% at 30% chord
Source UIUC Airfoil Coordinates Database

(n5h20-il) NACA 5-H-20 AIRFOIL

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NACA 5-H-20 AIRFOILNACA 5-H-20 rotorcraft airfoil
Max thickness 19.9% at 40% chord
Max camber 4.5% at 40% chord
Source UIUC Airfoil Coordinates Database

(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
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