Airfoil Tools
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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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(goe408-il) GOE 408 AIRFOIL

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GOE 408 AIRFOILGottingen 408 airfoil
Max thickness 7.8% at 30% chord
Max camber 4.1% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe409-il) GOE 409 AIRFOIL

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GOE 409 AIRFOILGottingen 409 airfoil
Max thickness 12.7% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(goe410-il) GOE 410 AIRFOIL

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GOE 410 AIRFOILGottingen 410 airfoil
Max thickness 16.1% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(goe411-il) GOE 411 AIRFOIL

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GOE 411 AIRFOILGottingen 411 airfoil
Max thickness 13.2% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(goe412-il) GOE 412 AIRFOIL

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GOE 412 AIRFOILGottingen 412 airfoil
Max thickness 13.1% at 29.7% chord
Max camber 5.1% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(goe413-il) GOE 413 AIRFOIL

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GOE 413 AIRFOILGottingen 413 airfoil
Max thickness 16.4% at 30% chord
Max camber 4.6% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe414-il) GOE 414 AIRFOIL

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GOE 414 AIRFOILGottingen 414 airfoil
Max thickness 13.6% at 29.7% chord
Max camber 5.3% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(goe415-il) GOE 415 AIRFOIL

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GOE 415 AIRFOILGottingen 415 airfoil
Max thickness 8.5% at 19.9% chord
Max camber 3.7% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe416a-il) GOE 416A AIRFOIL

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GOE 416A AIRFOILGottingen 416A airfoil
Max thickness 11.7% at 29.5% chord
Max camber 1.3% at 59.6% chord
Source UIUC Airfoil Coordinates Database

(goe417-il) GOE 417 AIRFOIL

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GOE 417 AIRFOILGottingen 417 airfoil
Max thickness 6% at 20% chord
Max camber 6.1% at 40% chord
Source UIUC Airfoil Coordinates Database
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