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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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(joukowsk0015-jf) Joukovsky f=0% t=15%

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Joukovsky f=0% t=15%Joukowski 15% symmetrical airfoil
Max thickness 15% at 24.6% chord
Max camber 0% at 0% chord
Source Javafoil generated

(naca0015-il) NACA 0015

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NACA 0015NACA 0015 airfoil
Max thickness 15% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx711520-il) FX 71-L-150/20 AIRFOIL

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FX 71-L-150/20 AIRFOILWortmann FX 71-L-150/20 airfoil
Max thickness 15% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx711525-il) FX 71-L-150/25 AIRFOIL

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FX 71-L-150/25 AIRFOILWortmann FX 71-L-150/25 airfoil
Max thickness 15% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx711530-il) FX 71-L-150/30 AIRFOIL

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FX 71-L-150/30 AIRFOILWortmann FX 71-L-150/30 airfoil
Max thickness 15% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(n64015-il) NACA 642-015 AIRFOIL

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NACA 642-015 AIRFOILNACA 64(2)-015 airfoil
Max thickness 15% at 35% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(lwk80150k25-il) LWK 80-150/K25

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LWK 80-150/K25LWK 80-150/K25 symmetrical airfoil
Max thickness 15% at 40.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx71l150-il) FX 71-L-150/30 AIRFOIL

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FX 71-L-150/30 AIRFOILWortmann FX 71-L-150/30 airfoil
Max thickness 15% at 33.9% 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

(n64015a-il) NACA 642-015A AIRFOIL

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NACA 642-015A AIRFOILNACA 64(2)-015A airfoil
Max thickness 15% at 40% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
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