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.
(fx63137-il) WORTMANN FX 63-137 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Wortmann FX 63-137 human power aircraft airfoil (Liver Puffin) airfoil Max thickness 13.7% at 30.9% chord Max camber 6% at 53.3% chord Max Cl/Cd 105.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe54-il) GOE 54 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 54 airfoil Max thickness 6.5% at 14.9% chord Max camber 3.5% at 19.9% chord Max Cl/Cd 105.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e682-il) EPPLER 682 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E682 sailplane airfoil Max thickness 15.3% at 40.4% chord Max camber 2.9% at 40.4% chord Max Cl/Cd 105.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(vr7b-il) BOEING-VERTOL VR-7 AIRFOIL WITH TAB | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Boeing-Vertol VR-7 rotorcraft airfoil with tab Max thickness 12% at 33% chord Max camber 3% at 29% chord Max Cl/Cd 105.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(hq209-il) HQ 2.0/9 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Quabeck HQ 2.0/9 R/C sailplane airfoil Max thickness 9% at 35% chord Max camber 2% at 50% chord Max Cl/Cd 105.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe244-il) GOE 244 (MVA PR.4) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 244 (MVA PR.4) airfoil Max thickness 17.7% at 19.6% chord Max camber 10% at 49.6% chord Max Cl/Cd 105.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe563-il) GOE 563 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 563 airfoil Max thickness 8.9% at 29.8% chord Max camber 2.2% at 49.8% chord Max Cl/Cd 105.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(sd7043-il) SD7043 (9.1%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Selig/Donovan SD7043 low Reynolds number airfoil Max thickness 9.1% at 26.6% chord Max camber 3.3% at 50.2% chord Max Cl/Cd 105.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(clarkv-il) CLARK V AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | CLARK V airfoil Max thickness 11.6% at 30% chord Max camber 3.4% at 50% chord Max Cl/Cd 105.6 at Re# 1,000,000 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 105.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database |
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