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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(goe398-il) GOE 398 AIRFOIL

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GOE 398 AIRFOILGottingen 398 airfoil
Max thickness 13.9% at 30% chord
Max camber 4.9% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe399-il) GOE 399 AIRFOIL

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GOE 399 AIRFOILGottingen 399 airfoil
Max thickness 6.9% at 29.9% chord
Max camber 4.2% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe400-il) GOE 400 AIRFOIL

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GOE 400 AIRFOILGottingen 400 airfoil
Max thickness 6.1% at 20% chord
Max camber 4.9% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe401-il) GOE 401 AIRFOIL

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GOE 401 AIRFOILGottingen 401 airfoil
Max thickness 7.1% at 29.9% chord
Max camber 4.9% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe402-il) GOE 402 AIRFOIL

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GOE 402 AIRFOILGottingen 402 airfoil
Max thickness 6.8% at 20% chord
Max camber 5.7% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe403-il) GOE 403 AIRFOIL

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GOE 403 AIRFOILGottingen 403 airfoil
Max thickness 6.7% at 29.9% chord
Max camber 4.3% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe404-il) GOE 404 AIRFOIL

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GOE 404 AIRFOILGottingen 404 airfoil
Max thickness 13.2% at 29.6% chord
Max camber 5% at 29.6% chord
Source UIUC Airfoil Coordinates Database

(goe405-il) GOE 405 AIRFOIL

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GOE 405 AIRFOILGottingen 405 airfoil
Max thickness 11.1% at 30% chord
Max camber 6.5% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe406-il) GOE 406 AIRFOIL

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GOE 406 AIRFOILGottingen 406 airfoil
Max thickness 11.7% at 29.9% chord
Max camber 5.5% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe407-il) GOE 407 AIRFOIL

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GOE 407 AIRFOILGottingen 407 airfoil
Max thickness 9.5% at 29.9% chord
Max camber 4.8% at 39.9% chord
Source UIUC Airfoil Coordinates Database
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