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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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(goe100-il) GOE 100 (SOPWITH) AIRFOIL

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GOE 100 (SOPWITH) AIRFOILGottingen 100 (Sopwith) airfoil
Max thickness 6.6% at 20% chord
Max camber 3.6% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe101-il) GOE 101 AIRFOIL

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GOE 101 AIRFOILGottingen 101 airfoil
Max thickness 6.9% at 30% chord
Max camber 4% at 30% chord
Source UIUC Airfoil Coordinates Database

(goe10k-il) GOE 10K AIRFOIL

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GOE 10K AIRFOILGottingen 10K airfoil
Max thickness 3.9% at 50% chord
Max camber 1.4% at 60% chord
Source UIUC Airfoil Coordinates Database

(goe113-il) GOE 113 AIRFOIL

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GOE 113 AIRFOILGottingen 113 airfoil
Max thickness 6.7% at 30% chord
Max camber 3% at 40% chord
Source UIUC Airfoil Coordinates Database

(goe114-il) GOE 114 (MVA MK.1) AIRFOIL

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GOE 114 (MVA MK.1) AIRFOILGottingen 114 (MVA MK.1) airfoil
Max thickness 9.6% at 29.7% chord
Max camber 3.5% at 49.7% chord
Source UIUC Airfoil Coordinates Database

(goe115-il) GOE 115 (MVA MK.2) AIRFOIL

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GOE 115 (MVA MK.2) AIRFOILGottingen 115 (MVA MK.2) airfoil
Max thickness 9.7% at 29.7% chord
Max camber 3.7% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(goe116-il) GOE 116 (MVA MK.3) AIRFOIL

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GOE 116 (MVA MK.3) AIRFOILGottingen 116 (MVA MK.3) airfoil
Max thickness 9.3% at 39.8% chord
Max camber 4.1% at 39.8% chord
Source UIUC Airfoil Coordinates Database

(goe117-il) GOE 117 (MVA MK.4) AIRFOIL

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GOE 117 (MVA MK.4) AIRFOILGottingen 117 (MVA MK.4) airfoil
Max thickness 9% at 29.8% chord
Max camber 4.6% at 39.8% chord
Source UIUC Airfoil Coordinates Database

(goe118-il) GOE 118 (MVA MK.7) AIRFOIL

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GOE 118 (MVA MK.7) AIRFOILGottingen 118 (MVA MK.7) airfoil
Max thickness 8.6% at 29.9% chord
Max camber 5.7% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(goe11k-il) GOE 11K AIRFOIL

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GOE 11K AIRFOILGottingen 11K airfoil
Max thickness 7.5% at 50% chord
Max camber 2.7% at 60% chord
Source UIUC Airfoil Coordinates Database
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