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.
(e793-il) EPPLER 793 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E793 general purpose airfoil (gyroflug speed canard canard) Max thickness 15.6% at 26.7% chord Max camber 4.2% at 44.7% chord Max Cl/Cd 43.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(eh1090-il) EH 1.0/9.0 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | John Yost EH 1.0/9.0 for tailless R/C aircraft Max thickness 9% at 28.7% chord Max camber 1% at 25.9% chord Max Cl/Cd 43.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(e549-il) EPPLER 549 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E549 general aviation airfoil Max thickness 18.1% at 38.7% chord Max camber 2% at 34% chord Max Cl/Cd 43.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(s823-nr) NREL's S823 Airfoil | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file | |
![]() | NREL HAWT airfoil S823 root 21.0% Dia=2 to 10 m Re=4.0E+5 Clmax(S)=1.20 Clmax(R)=1.16 Restrained max lift coef Max thickness 21.2% at 24.3% chord Max camber 2.4% at 70.5% chord Max Cl/Cd 43.2 at Re# 100,000 Source NWTC National WInd Technology Center | |
(s8038-il) S8038 (13%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Selig S8038 (13%) low Reynolds number airfoil Max thickness 13% at 32.9% chord Max camber 0.6% at 40.1% chord Max Cl/Cd 43.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe449-il) GOE 449 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 449 airfoil Max thickness 17% at 30% chord Max camber 5.4% at 40% chord Max Cl/Cd 43.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(r140-il) R140 (original) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | R140 Quickee 500 airfoil (original) Max thickness 12% at 39.3% chord Max camber 0.5% at 42.3% chord Max Cl/Cd 43.2 at Re# 100,000 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 43.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe648-il) GOE 648 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 648 airfoil Max thickness 15.2% at 29.4% chord Max camber 3.9% at 39.4% chord Max Cl/Cd 43.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(marske7-il) RONCZ LOW DRAG FLYING WING AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Roncz/Marske-7 low drag flying wing airfoil Max thickness 12.1% at 42.8% chord Max camber 2.8% at 39.1% chord Max Cl/Cd 43.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database |
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