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Airfoil database search

Search the 1638 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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(e559-il) EPPLER 559 AIRFOIL

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EPPLER 559 AIRFOILEppler E559 general aviation airfoil
Max thickness 16% at 27.2% chord
Max camber 4.3% at 50.2% chord
Source UIUC Airfoil Coordinates Database

(fx77w270-il) FX 77-W-270

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FX 77-W-270Wortmann FX 77-W-270 airfoil for use on wind turbines (W)
Max thickness 27.1% at 33.9% chord
Max camber 4.3% at 27.9% chord
Source UIUC Airfoil Coordinates Database

(fx77w258-il) WORTMANN FX 77-W-258 AIRFOIL

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WORTMANN FX 77-W-258 AIRFOILWortmann FX 77-W-258 wind turbine airfoil
Max thickness 26.1% at 30.9% chord
Max camber 4.3% at 27.9% chord
Source UIUC Airfoil Coordinates Database

(goe210-il) GOE 210 (DAIMLER) AIRFOIL

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GOE 210 (DAIMLER) AIRFOILGottingen 210 (DAIMLER) airfoil
Max thickness 6.6% at 30% chord
Max camber 4.3% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe328-il) GOE 328 AIRFOIL

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GOE 328 AIRFOILGottingen 328 airfoil
Max thickness 8.2% at 30% chord
Max camber 4.3% at 30% chord
Source UIUC Airfoil Coordinates Database

(e793-il) EPPLER 793 AIRFOIL

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EPPLER 793 AIRFOILEppler E793 general purpose airfoil (gyroflug speed canard canard)
Max thickness 15.6% at 26.7% chord
Max camber 4.2% at 44.7% chord
Source UIUC Airfoil Coordinates Database

(s804-nr) NREL's S804 Airfoil

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NREL's S804 AirfoilNREL HAWT airfoil S804 root Not recommended
Max thickness 17.9% at 26.7% chord
Max camber 4.2% at 39.6% chord
Source NWTC National WInd Technology Center

(fx84w150-il) FX 84-W-150

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FX 84-W-150Wortmann FX 84-W-150 airfoil for use on wind turbines (W)
Max thickness 15% at 37.1% chord
Max camber 4.2% at 40.2% chord
Source UIUC Airfoil Coordinates Database

(fx84w140-il) FX 84-W-140

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FX 84-W-140Wortmann FX 84-W-140 airfoil for use on wind turbines (W)
Max thickness 14.1% at 37.1% chord
Max camber 4.2% at 40.2% chord
Source UIUC Airfoil Coordinates Database

(goe316-il) GOE 316 (HANSA-BRANDENBURG IV.5) AIRFOIL

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GOE 316 (HANSA-BRANDENBURG IV.5) AIRFOILGottingen 316 (Hansa-Brandenburg IV.5) airfoil
Max thickness 9.1% at 29.9% chord
Max camber 4.2% at 29.9% chord
Source UIUC Airfoil Coordinates Database
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