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.
(goe315-il) GOE 315 (HANSA-BRANDENBURG III.5) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 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 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 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 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 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%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | 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 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Selig 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% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | 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 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 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 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 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 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 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 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 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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