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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(goe795sm-il) GOE 795 smoothed

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GOE 795 smoothedGottingen 795 airfoil (smoothed)
Max thickness 8% at 30.9% chord
Max camber 2.4% at 43.5% chord
Source UIUC Airfoil Coordinates Database

(goe796-il) GOE 796 AIRFOIL

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GOE 796 AIRFOILGottingen 796 airfoil
Max thickness 12% at 30% chord
Max camber 3.6% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe797-il) GOE 797 AIRFOIL

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GOE 797 AIRFOILGottingen 797 airfoil
Max thickness 16% at 30% chord
Max camber 4.9% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe798-il) GOE 798 AIRFOIL

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GOE 798 AIRFOILGottingen 798 airfoil
Max thickness 20% at 30% chord
Max camber 6% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe801-il) GOE 801 (MVA 301) AIRFOIL

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GOE 801 (MVA 301) AIRFOILGottingen 801 (MVA 301) airfoil
Max thickness 9.8% at 30% chord
Max camber 6.1% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe802-il) GOE 802 AIRFOIL

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GOE 802 AIRFOILGottingen 802 airfoil
Max thickness 9.8% at 30% chord
Max camber 6.1% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe802a-il) GOE 802 A AIRFOIL

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GOE 802 A AIRFOILGottingen 802 A airfoil
Max thickness 9.8% at 30% chord
Max camber 6.1% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe802b-il) GOE 802 B AIRFOIL

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GOE 802 B AIRFOILGottingen 802 B airfoil
Max thickness 9.8% at 30% chord
Max camber 6.1% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe803h-il) GOE 803 (HACKLINGER) AIRFOIL

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GOE 803 (HACKLINGER) AIRFOILGottingen 803 (Hacklinger) airfoil
Max thickness 6.3% at 15% chord
Max camber 6.6% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe804-il) GOE 804 (EA 8) AIRFOIL

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GOE 804 (EA 8) AIRFOILGottingen 804 (EA 8) airfoil
Max thickness 6% at 40% chord
Max camber 6.3% at 50% chord
Source UIUC Airfoil Coordinates Database
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