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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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(fx66h80-il) FX 66-H-80

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FX 66-H-80Wortmann FX 66-H-80 airfoil
Max thickness 8% at 27.9% chord
Max camber 2.5% at 25% chord
Max Cl/Cd 105.3 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database

(goe57-il) GOE 57 AIRFOIL

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GOE 57 AIRFOILGottingen 57 airfoil
Max thickness 6.3% at 19.9% chord
Max camber 5.1% at 39.9% chord
Max Cl/Cd 105.3 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database

(s812-nr) NREL's S812 Airfoil

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NREL's S812 AirfoilNREL HAWT airfoil S812 primary
Max thickness 21% at 39.6% chord
Max camber 1.6% at 77% chord
Max Cl/Cd 105.2 at Re# 1,000,000
Source NWTC National WInd Technology Center

(goe646-il) GOE 646 AIRFOIL

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GOE 646 AIRFOILGottingen 646 airfoil
Max thickness 18.3% at 29% chord
Max camber 4.5% at 49% chord
Max Cl/Cd 105.2 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database

(atr72sm-il) Smoothed ATR airfoil coordinates obtained using AFSMO (Harry Morgan's NASA smoothing program)

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Smoothed ATR airfoil coordinates obtained  using AFSMO (Harry Morgan's NASA smoothing program)ATR 72 wing airfoil (from NTSB report)
Max thickness 14.5% at 25.4% chord
Max camber 2.9% at 21.4% chord
Max Cl/Cd 105.2 at Re# 1,000,000
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
Max Cl/Cd 105.2 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database

(ag35-il) AG35

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AG35Drela AG35 airfoil
Max thickness 8.7% at 27.9% chord
Max camber 2.3% at 37% chord
Max Cl/Cd 105.2 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database

(e556-il) EPPLER 556 AIRFOIL

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EPPLER 556 AIRFOILEppler E556 general aviation airfoil
Max thickness 16% at 31.1% chord
Max camber 3.1% at 61.4% chord
Max Cl/Cd 105.2 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database

(fg2-il) Fage & Collins 2

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Fage & Collins 2Fage & Collins 2 airfoil
Max thickness 8.2% at 30% chord
Max camber 3.3% at 30% chord
Max Cl/Cd 105.2 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database

(goe377-il) GOE 377 AIRFOIL

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GOE 377 AIRFOILGottingen 377 airfoil
Max thickness 6.5% at 30% chord
Max camber 3.9% at 40% chord
Max Cl/Cd 105.2 at Re# 1,000,000
Source UIUC Airfoil Coordinates Database
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