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.
(goe584-il) GOE 584 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 584 airfoil Max thickness 12.7% at 30% chord Max camber 5% at 40% chord Max Cl/Cd 137.5 at Re# 1,000,000 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 137.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(gu255118-il) UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | University of Glasgow GU 25-5(11)8 canard airfoil (Quickie Max thickness 20% at 40% chord Max camber 7.1% at 45% chord Max Cl/Cd 137.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(fx66s196-il) FX 66-S-196 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 66-S-196 airfoil Max thickness 19.6% at 37.1% chord Max camber 3.8% at 43.5% chord Max Cl/Cd 137.4 at Re# 1,000,000 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 137.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe483-il) GOE 483 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 483 airfoil Max thickness 5.5% at 15% chord Max camber 5.8% at 40% chord Max Cl/Cd 137.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e420-il) EPPLER 420 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E420 high lift airfoil Max thickness 14.3% at 22.8% chord Max camber 10.6% at 40.5% chord Max Cl/Cd 137.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(fx73cl1152-il) FX 73-CL1-152 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 73-CL1-152 airfoil Max thickness 15.2% at 22.2% chord Max camber 6.1% at 33.9% chord Max Cl/Cd 137.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe303-il) GOE 303 (FRIEDRICHSHAFEN G03) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 303 (Friedrichshafen G03) airfoil Max thickness 9.8% at 29.9% chord Max camber 5.9% at 39.9% chord Max Cl/Cd 137.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(s817-nr) NREL's S817 Airfoil | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file | |
 | NREL HAWT airfoil S817 tip 16.0% Dia=30 to 50 m Re=3.0E+6 Clmax(S)=1.10 Clmax(R)=1.08 Restrained max lift coef Max thickness 16% at 51.1% chord Max camber 2.8% at 41.1% chord Max Cl/Cd 137.3 at Re# 1,000,000 Source NWTC National WInd Technology Center | |
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