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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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(goe315-il) GOE 315 (HANSA-BRANDENBURG III.5) AIRFOIL

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GOE 315 (HANSA-BRANDENBURG III.5) AIRFOILGottingen 315 (Hansa-Brandenburg III.5) airfoil
Max thickness 8.1% at 29.9% chord
Max camber 4.1% at 29.9% chord
Max Cl/Cd 55.8 at Re# 100,000
Source UIUC Airfoil Coordinates Database

(goe412-il) GOE 412 AIRFOIL

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GOE 412 AIRFOILGottingen 412 airfoil
Max thickness 13.1% at 29.7% chord
Max camber 5.1% at 39.7% chord
Max Cl/Cd 55.8 at Re# 100,000
Source UIUC Airfoil Coordinates Database

(goe274-il) GOE 274 (DAIMLER V) AIRFOIL

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GOE 274 (DAIMLER V) AIRFOILGottingen 274 (DAIMLER V) airfoil
Max thickness 8.7% at 29.9% chord
Max camber 4.8% at 29.9% chord
Max Cl/Cd 55.8 at Re# 100,000
Source UIUC Airfoil Coordinates Database

(e222-il) E222 (10.17%)

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E222  (10.17%)Eppler E222 low Reynolds number airfoil
Max thickness 10.2% at 31.1% chord
Max camber 2.1% at 55.3% chord
Max Cl/Cd 55.8 at Re# 100,000
Source UIUC Airfoil Coordinates Database

(s3002-il) SELIG 3002-099-83

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SELIG 3002-099-83Selig S3002 low Reynolds number airfoil
Max thickness 9.9% at 30.6% chord
Max camber 2.3% at 49.8% chord
Max Cl/Cd 55.8 at Re# 100,000
Source UIUC Airfoil Coordinates Database

(mh117-il) MH 117 9.8%

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MH 117  9.8%Martin Hepperle MH 117 for a propeller for ultralight (tip)
Max thickness 9.8% at 29.1% chord
Max camber 2.7% at 44.6% chord
Max Cl/Cd 55.8 at Re# 100,000
Source UIUC Airfoil Coordinates Database

(goe431-il) GOE 431 AIRFOIL

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GOE 431 AIRFOILGottingen 431 airfoil
Max thickness 11.8% at 20% chord
Max camber 7.2% at 60% chord
Max Cl/Cd 55.7 at Re# 100,000
Source UIUC Airfoil Coordinates Database

(goe301-il) GOE 301 (FRIEDRICHSHAFEN G 13) AIRFOIL

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GOE 301 (FRIEDRICHSHAFEN G 13) AIRFOILGottingen 301 (Friedrichshafen G 13) airfoil
Max thickness 10% at 28.9% chord
Max camber 6.5% at 39.9% chord
Max Cl/Cd 55.7 at Re# 100,000
Source UIUC Airfoil Coordinates Database

(goe321-il) GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL

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GOE 321 (HANSA-BRANDENBURG III.1) AIRFOILGottingen 321 (Hansa-Brandenburg III.1) airfoil
Max thickness 11.2% at 29.9% chord
Max camber 5.1% at 29.9% chord
Max Cl/Cd 55.7 at Re# 100,000
Source UIUC Airfoil Coordinates Database

(goe277-il) GOE 277 (DAIMLER VIII) AIRFOIL

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GOE 277 (DAIMLER VIII) AIRFOILGottingen 277 (DAIMLER VIII) airfoil
Max thickness 8.3% at 29.9% chord
Max camber 4.4% at 29.9% chord
Max Cl/Cd 55.7 at Re# 100,000
Source UIUC Airfoil Coordinates Database
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