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.
(m17-il) NACA M17 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | NACA/Munk M-17 airfoil Max thickness 8.1% at 40% chord Max camber 4.1% at 30% chord Max Cl/Cd 74.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(goe308-il) GOE 308 (MVA H.40) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 308 (MVA H.40) airfoil Max thickness 8.1% at 29.9% chord Max camber 5% at 29.9% chord Max Cl/Cd 74.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(mh18-il) MH 18 11.16% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Martin Hepperle MH 18 for F3D Pylon Racing Max thickness 11.1% at 36.8% chord Max camber 2.7% at 42.1% chord Max Cl/Cd 74.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(ah80140-il) AH 80-140 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Althaus AH 80-140 airfoil Max thickness 14% at 30.9% chord Max camber 4.4% at 33.9% chord Max Cl/Cd 74.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(goe324-il) GOE 324 (HANSA-BRANDENBURG) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 324 (Hansa-Brandenburg) airfoil Max thickness 13.1% at 29.8% chord Max camber 5.9% at 29.8% chord Max Cl/Cd 74.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(goe142-il) GOE 142 (MVA H.19) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 142 (MVA H.19) airfoil Max thickness 6.2% at 24.9% chord Max camber 3.8% at 34.9% chord Max Cl/Cd 74.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(m13-il) NACA M13 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | NACA/Munk M-13 airfoil Max thickness 6.2% at 30% chord Max camber 3.8% at 30% chord Max Cl/Cd 74.1 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(goe401-il) GOE 401 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 401 airfoil Max thickness 7.1% at 29.9% chord Max camber 4.9% at 29.9% chord Max Cl/Cd 74.1 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(e561-il) EPPLER 561 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E561 general aviation airfoil Max thickness 16.9% at 27.9% chord Max camber 5.1% at 45.8% chord Max Cl/Cd 74.1 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(usa25-il) USA 25 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | USA-25 airfoil Max thickness 8.3% at 19.9% chord Max camber 5.2% at 29.9% chord Max Cl/Cd 74.1 at Re# 200,000 Source UIUC Airfoil Coordinates Database |
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