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Airfoil database list (N).

NACA 0018 to NACA 2408

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(naca0018-il) NACA 0018

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NACA 0018NACA 0018 airfoil
Max thickness 18% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca0021-il) NACA 0021

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NACA 0021NACA 0021 airfoil
Max thickness 21% at 30% 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

(naca1408-il) NACA 1408

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NACA 1408NACA 1408 airfoil
Max thickness 8% at 30% chord
Max camber 1% at 40% chord
Source UIUC Airfoil Coordinates Database

(naca1410-il) NACA 1410

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NACA 1410NACA 1410 airfoil
Max thickness 10% at 29.9% chord
Max camber 1% at 50% chord
Source UIUC Airfoil Coordinates Database

(naca1412-il) NACA 1412

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NACA 1412NACA 1412 airfoil
Max thickness 12% at 29.9% chord
Max camber 1% at 40% chord
Source UIUC Airfoil Coordinates Database

(naca16006-il) NACA 16-006

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NACA 16-006NACA 16-006 airfoil
Max thickness 6% at 50% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca16009-il) NACA 16009

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NACA 16009NACA 16009 airfoil
Max thickness 9% at 50% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca16012-il) NACA 16-012

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NACA 16-012NACA 16-012 airfoil
Max thickness 12% at 50% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca16015-il) NACA 16-015

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NACA 16-015NACA 16-015 airfoil
Max thickness 15% at 50% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca16018-il) NACA 16-018

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NACA 16-018NACA 16-018 airfoil
Max thickness 18% at 50% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca16021-il) NACA 16-021

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NACA 16-021NACA 16-021 airfoil
Max thickness 21% at 50% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca22112-jf) NACA 22112

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NACA 22112NACA 22112 5 digit reflex airfoil
Max thickness 12% at 29.5% chord
Max camber 0.8% at 9.6% chord
Source Javafoil generated

(naca23012-il) NACA 23012 12%

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NACA 23012  12%NACA 23012 airfoil
Max thickness 12% at 29.8% chord
Max camber 1.8% at 12.7% chord
Source UIUC Airfoil Coordinates Database

(naca23015-il) NACA 23015

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NACA 23015NACA 23015 airfoil
Max thickness 15% at 30% chord
Max camber 1.8% at 15% chord
Source UIUC Airfoil Coordinates Database

(naca23018-il) NACA 23018

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NACA 23018NACA 23018 airfoil
Max thickness 18% at 30% chord
Max camber 1.8% at 15% chord
Source UIUC Airfoil Coordinates Database

(naca23021-il) NACA 23021

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NACA 23021NACA 23021 airfoil
Max thickness 21% at 30% chord
Max camber 1.9% at 10% chord
Source UIUC Airfoil Coordinates Database

(naca23024-il) NACA 23024

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NACA 23024NACA 23024 airfoil
Max thickness 24% at 30.3% chord
Max camber 2.9% at 1.3% chord
Source UIUC Airfoil Coordinates Database

(naca23112-jf) NACA 23112

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NACA 23112NACA 23112 5 digit reflex airfoil
Max thickness 12% at 29.5% chord
Max camber 1.2% at 14.7% chord
Source Javafoil generated

(naca2408-il) NACA 2408

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NACA 2408NACA 2408 airfoil
Max thickness 8% at 29.9% chord
Max camber 2% at 40% chord
Source UIUC Airfoil Coordinates Database
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