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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(goe567-il) GOE 567 AIRFOIL

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GOE 567 AIRFOILGottingen 567 airfoil
Max thickness 14.8% at 29.5% chord
Max camber 5.3% at 49.5% chord
Source UIUC Airfoil Coordinates Database

(goe57-il) GOE 57 AIRFOIL

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GOE 57 AIRFOILGottingen 57 airfoil
Max thickness 6.3% at 19.9% chord
Max camber 5.1% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe570-il) GOE 570 AIRFOIL

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GOE 570 AIRFOILGottingen 570 airfoil
Max thickness 33.7% at 30% chord
Max camber 9.7% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe571-il) GOE 571 AIRFOIL

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GOE 571 AIRFOILGottingen 571 airfoil
Max thickness 24.9% at 29.4% chord
Max camber 9.8% at 29.4% chord
Source UIUC Airfoil Coordinates Database

(goe572-il) GOE 572 AIRFOIL

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GOE 572 AIRFOILGottingen 572 airfoil
Max thickness 18.6% at 29.9% chord
Max camber 8.3% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe573-il) GOE 573 AIRFOIL

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GOE 573 AIRFOILGottingen 573 airfoil
Max thickness 14.1% at 29.9% chord
Max camber 6.5% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe574-il) GOE 574 AIRFOIL

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GOE 574 AIRFOILGottingen 574 airfoil
Max thickness 10.3% at 30% chord
Max camber 4.9% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe575-il) GOE 575 AIRFOIL

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GOE 575 AIRFOILGottingen 575 airfoil
Max thickness 13.3% at 29.8% chord
Max camber 3.6% at 39.8% chord
Source UIUC Airfoil Coordinates Database

(goe584-il) GOE 584 AIRFOIL

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GOE 584 AIRFOILGottingen 584 airfoil
Max thickness 12.7% at 30% chord
Max camber 5% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe585-il) GOE 585 AIRFOIL

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GOE 585 AIRFOILGottingen 585 airfoil
Max thickness 8.2% at 20% chord
Max camber 3.4% at 40% chord
Source UIUC Airfoil Coordinates Database
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