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.
(fx84w127-il) FX 84-W-127 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 84-W-127 airfoil for use on wind turbines (W) Max thickness 12.8% at 33.9% chord Max camber 3.7% at 40.2% chord Max Cl/Cd 115.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(e377m-il) EPPLER 377 (MODIFIED) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E377 (modified) ultralight airfoil Max thickness 3.8% at 6.1% chord Max camber 9.2% at 32.6% chord Max Cl/Cd 115.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe456-il) GOE 456 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 456 airfoil Max thickness 7.2% at 29.9% chord Max camber 5.2% at 39.9% chord Max Cl/Cd 115.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(fx74cl5140-il) FX74_CL5_140 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 74-CL5-140 high lift airfoil Max thickness 14% at 30.9% chord Max camber 9.9% at 37.1% chord Max Cl/Cd 115.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(fx77w121-il) FX 77-W-121 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 77-W-121 airfoil for use on wind turbines (W) Max thickness 12.1% at 30.9% chord Max camber 4.6% at 30.9% chord Max Cl/Cd 115.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe405-il) GOE 405 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 405 airfoil Max thickness 11.1% at 30% chord Max camber 6.5% at 40% chord Max Cl/Cd 115.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(ah63k127-il) AH 63-K-127/24 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Althaus AH 63-K-127/24 airfoil for use with flaps (K) Max thickness 12.7% at 40.2% chord Max camber 3.8% at 43.5% chord Max Cl/Cd 115.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(sd6080-il) SD6080 (9.2%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Selig/Donovan SD6080 low Reynolds number airfoil Max thickness 9.2% at 30.9% chord Max camber 3.2% at 44.7% chord Max Cl/Cd 115.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe458-il) GOE 458 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 458 airfoil Max thickness 7.2% at 29.9% chord Max camber 5.2% at 39.9% chord Max Cl/Cd 115.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(e593-il) EPPLER 593 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E593 airfoil Max thickness 11.3% at 24.2% chord Max camber 4.6% at 29.2% chord Max Cl/Cd 115.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
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