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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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(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

(e521-il) EPPLER 521 AIRFOIL

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EPPLER 521 AIRFOILEppler E521 tailplane airfoil
Max thickness 13.8% at 37% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s8035-il) S8035 for RC aerobatic 14% thick

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S8035 for RC aerobatic  14% thickSelig S8035 low Reynolds number airfoil
Max thickness 14% at 29.1% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s1048-il) S1048 14% (Danny Howell)

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S1048 14% (Danny Howell)Selig S1048 airfoil
Max thickness 14% at 27% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e474-il) E474 (14.09%)

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E474  (14.09%)Eppler E474 aerobatic aircraft airfoil
Max thickness 14.1% at 21.5% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fxl142k-il) FX LIII-142 K 25 AIRFOIL

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FX LIII-142 K 25 AIRFOILWortmann FX LIII-142 K 25 airfoil
Max thickness 14.2% at 30.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e169-il) E169 (14.4%)

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E169  (14.4%)Eppler E169 low Reynolds number airfoil
Max thickness 14.4% at 26.5% 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

(e520-il) EPPLER 520 AIRFOIL

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EPPLER 520 AIRFOILEppler E520 tailplane airfoil
Max thickness 15% at 36.7% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e475-il) E475 (15.01%)

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E475  (15.01%)Eppler E475 aerobatic aircraft airfoil
Max thickness 15% at 21.7% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
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