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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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(goe704-il) GOE 704 AIRFOIL

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GOE 704 AIRFOILGottingen 704 airfoil
Max thickness 12.9% at 29.9% chord
Max camber 2.1% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe711-il) GOE 711 AIRFOIL

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GOE 711 AIRFOILGottingen 711 airfoil
Max thickness 14.9% at 30% chord
Max camber 6.3% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe723-il) GOE 723 AIRFOIL

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GOE 723 AIRFOILGottingen 723 airfoil
Max thickness 11.6% at 29.7% chord
Max camber 4.5% at 49.7% chord
Source UIUC Airfoil Coordinates Database

(goe735-il) GOE 735 AIRFOIL

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GOE 735 AIRFOILGottingen 735 airfoil
Max thickness 20.1% at 30% chord
Max camber 4.4% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe738-il) GOE 738 AIRFOIL

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GOE 738 AIRFOILGottingen 738 airfoil
Max thickness 15.4% at 30% chord
Max camber 2.1% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe741-il) GOE 741 AIRFOIL

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GOE 741 AIRFOILGottingen 741 airfoil
Max thickness 15.3% at 30% chord
Max camber 4.8% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe744-il) GOE 744 AIRFOIL

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GOE 744 AIRFOILGottingen 744 airfoil
Max thickness 14.5% at 20% chord
Max camber 7% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe746-il) GOE 746 AIRFOIL

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GOE 746 AIRFOILGottingen 746 airfoil
Max thickness 9.8% at 30% chord
Max camber 5% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe758-il) GOE 758 AIRFOIL

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GOE 758 AIRFOILGottingen 758 airfoil
Max thickness 13.9% at 30% chord
Max camber 4.7% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe765-il) Gottingen 765 airfoil (recovered). Thick: .144 LE radius: 0.02062 LE slope: 0.17300

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Gottingen 765 airfoil (recovered). Thick: .144 LE radius: 0.02062 LE slope: 0.17300Used on the Me163 Komet
Max thickness 14.4% at 30% chord
Max camber 1.9% at 25.9% chord
Source UIUC Airfoil Coordinates Database
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