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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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(e421-il) EPPLER 421 AIRFOIL

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EPPLER 421 AIRFOILEppler E421 high lift airfoil
Max thickness 14.5% at 26% chord
Max camber 8.6% at 37.4% chord
Source UIUC Airfoil Coordinates Database

(e422-il) EPPLER 422 AIRFOIL

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EPPLER 422 AIRFOILEppler E422 high lift airfoil
Max thickness 14% at 24.1% chord
Max camber 7.1% at 34.8% chord
Source UIUC Airfoil Coordinates Database

(e426-il) EPPLER 426 AIRFOIL

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EPPLER 426 AIRFOILEppler E426 airfoil
Max thickness 10.8% at 25.5% chord
Max camber 0.6% at 50.6% chord
Source UIUC Airfoil Coordinates Database

(e428-il) EPPLER 428 AIRFOIL

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EPPLER 428 AIRFOILEppler E428 airfoil
Max thickness 11.1% at 17.2% chord
Max camber 0.5% at 50.6% chord
Source UIUC Airfoil Coordinates Database

(e431-il) EPPLER 431 AIRFOIL

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EPPLER 431 AIRFOILEppler E431 sailplane airfoil
Max thickness 15.1% at 37.4% chord
Max camber 4.2% at 42.6% chord
Source UIUC Airfoil Coordinates Database

(e432-il) EPPLER 432 AIRFOIL

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EPPLER 432 AIRFOILEppler E432 sailplane airfoil
Max thickness 16% at 37.4% chord
Max camber 4.5% at 37.4% chord
Source UIUC Airfoil Coordinates Database

(e433-il) EPPLER 433 AIRFOIL

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EPPLER 433 AIRFOILEppler E433 sailplane airfoil
Max thickness 14.2% at 42.6% chord
Max camber 3.9% at 42.6% chord
Source UIUC Airfoil Coordinates Database

(e434-il) EPPLER 434 AIRFOIL

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EPPLER 434 AIRFOILEppler E434 sailplane airfoil
Max thickness 13.3% at 38.6% chord
Max camber 4.3% at 38.6% chord
Source UIUC Airfoil Coordinates Database

(e435-il) EPPLER 435 AIRFOIL

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EPPLER 435 AIRFOILEppler E435 sailplane airfoil
Max thickness 16.2% at 40.9% chord
Max camber 4.4% at 56.2% chord
Source UIUC Airfoil Coordinates Database

(e472-il) EPPLER 472 AIRFOIL

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EPPLER 472 AIRFOILEppler E472 aerobatic aircraft airfoil
Max thickness 12.1% at 17.5% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
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