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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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(goe165-il) GOE 165 (MVA MK.11) AIRFOIL

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GOE 165 (MVA MK.11) AIRFOILGottingen 165 (MVA MK.11) airfoil
Max thickness 12.1% at 19.7% chord
Max camber 5.7% at 49.7% chord
Source UIUC Airfoil Coordinates Database

(goe167-il) GOE 167 (V.KARMAN PROP.2) AIRFOIL

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GOE 167 (V.KARMAN PROP.2) AIRFOILGottingen 167 (V.Karman PROP.2) airfoil
Max thickness 10.1% at 29.9% chord
Max camber 4.5% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe16k-il) GOE 16K AIRFOIL

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GOE 16K AIRFOILGottingen 16K airfoil
Max thickness 18.2% at 50% chord
Max camber 4.1% at 50% chord
Source UIUC Airfoil Coordinates Database

(goe173-il) GOE 173 (ALBATROS 6020) AIRFOIL

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GOE 173 (ALBATROS 6020) AIRFOILGottingen 173 (Albatros 6020) airfoil
Max thickness 7.8% at 20% chord
Max camber 5.9% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe174-il) GOE 174 (ALBATROS 5020) AIRFOIL

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GOE 174 (ALBATROS 5020) AIRFOILGottingen 174 (Albatros 5020) airfoil
Max thickness 8.6% at 19.9% chord
Max camber 5.6% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe176-il) GOE 176 (ALBATROS 7020) AIRFOIL

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GOE 176 (ALBATROS 7020) AIRFOILGottingen 176 (Albatros 7020) airfoil
Max thickness 10.3% at 19.8% chord
Max camber 5.6% at 39.8% chord
Source UIUC Airfoil Coordinates Database

(goe177-il) GOE 177 AIRFOIL

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GOE 177 AIRFOILGottingen 177 airfoil
Max thickness 7.7% at 20% chord
Max camber 5% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe178-il) GOE 178 AIRFOIL

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GOE 178 AIRFOILGottingen 178 airfoil
Max thickness 8.5% at 30% chord
Max camber 4.4% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe180-il) GOE 180 (MVA H.26) AIRFOIL

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GOE 180 (MVA H.26) AIRFOILGottingen 180 (MVA H.26) airfoil
Max thickness 8.7% at 30% chord
Max camber 4.4% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe182-il) GOE 182 (MVA H.27) AIRFOIL

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GOE 182 (MVA H.27) AIRFOILGottingen 182 (MVA H.27) airfoil
Max thickness 9.5% at 19.9% chord
Max camber 5.3% at 39.9% chord
Source UIUC Airfoil Coordinates Database
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