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Airfoil database search (Symmetrical)

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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(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

(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

(naca64a010-il) NACA 64A-010 10.0%

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NACA 64A-010 10.0%NACA 64A010 airfoil
Max thickness 10% at 40% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca66-018-il) NACA 66-018

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NACA 66-018NACA 66-018 airfoil
Max thickness 18% at 45% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(nacam2-il) NACA M2

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NACA M2NACA M2 airfoil
Max thickness 8.1% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(nacam3-il) NACA M3

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NACA M3NACA M3 airfoil
Max thickness 11.9% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(oaf139-il) OAF139 AIRFOIL

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OAF139 AIRFOILONERA/Aerospatiale OAF139 Fenestron airfoil
Max thickness 13.7% at 23.2% chord
Max camber 0% at 0.1% chord
Source UIUC Airfoil Coordinates Database

(prandtl-d-tip-ns) Prandtl-D tip - NASA Preliminary Research Aerodynamic Design To Lower Drag

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Prandtl-D tip - NASA Preliminary Research Aerodynamic Design To Lower DragNASA Preliminary Research Aerodynamic Design To Lower Drag (PRANDTL-D) glider tip airfoil
Max thickness 9.6% at 26.8% chord
Max camber 0% at 0% chord
Source NASA
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