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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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(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

(e471-il) E471 (6.25%)

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E471  (6.25%)Eppler E471 airfoil
Max thickness 6.3% at 29.8% chord
Max camber 4.5% at 53.5% 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

(e473-il) EPPLER 473 AIRFOIL

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EPPLER 473 AIRFOILEppler E473 aerobatic aircraft airfoil
Max thickness 16.2% at 21.2% 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

(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

(e479-il) EPPLER 479 AIRFOIL

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EPPLER 479 AIRFOILEppler E479 aerobatic aircraft airfoil
Max thickness 16.6% at 25.7% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e485-il) EPPLER 485 AIRFOIL

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EPPLER 485 AIRFOILEppler E485 tailplane airfoil
Max thickness 12.5% at 31.8% chord
Max camber 1.1% at 27.1% chord
Source UIUC Airfoil Coordinates Database
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