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.
(e838-il) EPPLER E838 HYDROFOIL AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E838 hydrofoil Max thickness 18.4% at 37.2% chord Max camber 0% at 46.5% chord Max Cl/Cd 31.5 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(e637-il) EPPLER 637 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E637 airfoil Max thickness 12.1% at 27.6% chord Max camber 3.6% at 23.6% chord Max Cl/Cd 31.5 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(e344-il) EPPLER 344 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E344 flying wing airfoil Max thickness 14.7% at 29.9% chord Max camber 4.3% at 25% chord Max Cl/Cd 31.5 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(e748-il) EPPLER 748 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E748 sailplane airfoil Max thickness 19.7% at 27.4% chord Max camber 4.6% at 54.9% chord Max Cl/Cd 31.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe421-il) GOE 421 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 421 airfoil Max thickness 19% at 29.3% chord Max camber 8.1% at 49.3% chord Max Cl/Cd 31.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(ah83159-il) AH 83-159 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Althaus AH 83-159 airfoil Max thickness 15.9% at 40.2% chord Max camber 3.8% at 40.2% chord Max Cl/Cd 31.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(cp-100-050-gn) Cambered plate C=10% T=5% R=1.3 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file | |
![]() | HAWT pipe blade with coordinates based on top surface. Camber=10% Wall thickness=5% Radius=1.3 Max thickness 7% at 4.2% chord Max camber 7.9% at 46.5% chord Max Cl/Cd 31.4 at Re# 100,000 Source Generated | |
(hq07-il) HQ 0/7 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Quabeck HQ 0/7 R/C sailplane airfoil Max thickness 7% at 33.9% chord Max camber 0% at 0% chord Max Cl/Cd 31.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(fx83w227-il) FX 83-W-227 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Wortmann FX 83-W-227 airfoil for use on wind turbines (W) Max thickness 22.6% at 33.9% chord Max camber 3.4% at 40.2% chord Max Cl/Cd 31.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(dae11-il) DAE-11 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Drela DAE11 low Reynolds number airfoil Max thickness 12.8% at 32.8% chord Max camber 6.6% at 44.4% chord Max Cl/Cd 31.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database |
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