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.
(goe81-il) GOE 81 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 81 airfoil Max thickness 7.4% at 29.9% chord Max camber 6.3% at 29.9% chord Max Cl/Cd 104.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(raf6-il) RAF 6 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | RAF-6 airfoil Max thickness 10% at 30% chord Max camber 4.6% at 30% chord Max Cl/Cd 104.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(ah81131-il) AH 81-131 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Althaus AH 81-131 airfoil Max thickness 13.1% at 40.2% chord Max camber 2.8% at 40.2% chord Max Cl/Cd 104.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(raf19-il) RAF 19 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | RAF-19 airfoil Max thickness 10.5% at 15% chord Max camber 10.1% at 40% chord Max Cl/Cd 104.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe430-il) GOE 430 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 430 airfoil Max thickness 13.4% at 29.5% chord Max camber 4.8% at 49.6% chord Max Cl/Cd 104.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe363-il) GOE 363 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 363 airfoil Max thickness 11.1% at 19.8% chord Max camber 5.7% at 39.8% chord Max Cl/Cd 104.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(s814-nr) NREL's S814 Airfoil | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file | |
 | NREL HAWT airfoil S814 root 24.0% Dia=20 to 30 m Re=1.5E+6 Clmax(S)=1.56 Clmax(R)=1.51 High max lift coef Max thickness 24.1% at 28.4% chord Max camber 3% at 74.5% chord Max Cl/Cd 104.7 at Re# 1,000,000 Source NWTC National WInd Technology Center | |
(goe391-il) GOE 391 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 391 airfoil Max thickness 5.1% at 40% chord Max camber 3.2% at 40% chord Max Cl/Cd 104.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe547-il) GOE 547 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 547 airfoil Max thickness 10.5% at 29.7% chord Max camber 4% at 49.7% chord Max Cl/Cd 104.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(marske1-il) MARSKE XM-1D AIRFOIL (F14-3.0) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Marske XM-1D airfoil (F14-3.0) Max thickness 14% at 25.1% chord Max camber 3% at 25.1% chord Max Cl/Cd 104.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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