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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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(e407-il) EPPLER 407 AIRFOIL

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EPPLER 407 AIRFOILEppler E407 sailplane airfoil
Max thickness 14.4% at 36.6% chord
Max camber 3.5% at 71.7% chord
Source UIUC Airfoil Coordinates Database

(e417-il) EPPLER 417 AIRFOIL

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EPPLER 417 AIRFOILEppler E417 general purpose airfoil
Max thickness 14.2% at 38.3% chord
Max camber 3.1% at 76.3% chord
Source UIUC Airfoil Coordinates Database

(e420-il) EPPLER 420 AIRFOIL

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EPPLER 420 AIRFOILEppler E420 high lift airfoil
Max thickness 14.3% at 22.8% chord
Max camber 10.6% at 40.5% chord
Source UIUC Airfoil Coordinates Database

(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

(e423-il) E423

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E423Eppler E423 high lift airfoil
Max thickness 12.5% at 23.7% chord
Max camber 9.5% at 41.4% 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
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