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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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(goe81-il) GOE 81 AIRFOIL

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GOE 81 AIRFOILGottingen 81 airfoil
Max thickness 7.4% at 29.9% chord
Max camber 6.3% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(goe92-il) GOE 92 AIRFOIL

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GOE 92 AIRFOILGottingen 92 airfoil
Max thickness 8.8% at 30% chord
Max camber 5.5% at 30% chord
Source UIUC Airfoil Coordinates Database

(gu255118-il) UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL

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UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOILUniversity of Glasgow GU 25-5(11)8 canard airfoil (Quickie
Max thickness 20% at 40% chord
Max camber 7.1% at 45% chord
Source UIUC Airfoil Coordinates Database

(sa7024-il) SA7024

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SA7024Selig / Ashok Gopalarathnam SA7024 low Reynolds number airfoil
Max thickness 7% at 25.9% chord
Max camber 3.3% at 43.3% chord
Source UIUC Airfoil Coordinates Database

(sa7025-il) SA7025

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SA7025Selig / Ashok Gopalarathnam SA7025 low Reynolds number airfoil
Max thickness 8% at 29.2% chord
Max camber 3.6% at 43.2% chord
Source UIUC Airfoil Coordinates Database

(sa7026-il) SA7026

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SA7026Selig / Ashok Gopalarathnam SA7026 low Reynolds number airfoil
Max thickness 9% at 32.9% chord
Max camber 3.8% at 47.1% chord
Source UIUC Airfoil Coordinates Database

(sa7035-il) SA7035

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SA7035Selig / Ashok Gopalarathnam SA7035
Max thickness 9.2% at 27.9% chord
Max camber 2.4% at 41.9% chord
Source UIUC Airfoil Coordinates Database

(sa7036-il) SA7036

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SA7036Selig / Ashok Gopalarathnam SA7036
Max thickness 9.2% at 28.1% chord
Max camber 2.6% at 42.1% chord
Source UIUC Airfoil Coordinates Database

(sa7038-il) SA7038

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SA7038Selig / Ashok Gopalarathnam SA7038
Max thickness 9.2% at 28.5% chord
Max camber 3% at 42.5% chord
Source UIUC Airfoil Coordinates Database

(ua2-180-il) UA(2)-180 (University of Alberta/Marsden)

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UA(2)-180 (University of Alberta/Marsden)UA(2)-180 airfoil for ultralight category aircraft
Max thickness 18.1% at 31.5% chord
Max camber 7% at 36.6% chord
Source UIUC Airfoil Coordinates Database
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