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.
(goe198-il) GOE 198 (L.F.G. 5294) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 198 (L.F.G. 5294) airfoil Max thickness 7.8% at 19.9% chord Max camber 6.5% at 39.9% chord Max Cl/Cd 64.5 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(fx63137sm-il) FX 63-137 13.7% smoothed | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 63-137 airfoil (smoothed) Max thickness 13.7% at 30.9% chord Max camber 5.8% at 56.5% chord Max Cl/Cd 64.5 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe394-il) GOE 394 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 394 airfoil Max thickness 6.1% at 19.9% chord Max camber 5.9% at 39.9% chord Max Cl/Cd 64.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe195-il) GOE 195 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 195 airfoil Max thickness 8.6% at 20% chord Max camber 5.1% at 50% chord Max Cl/Cd 64.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe450-il) GOE 450 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 450 airfoil Max thickness 8.9% at 29.9% chord Max camber 5.2% at 39.9% chord Max Cl/Cd 64.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe500-il) GOE 500 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 500 airfoil Max thickness 10% at 30% chord Max camber 6% at 50% chord Max Cl/Cd 64.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(cr001sm-il) cr001sm | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Cody Robertson CR 001 R/C hand-launch low Reynolds number airfoil (smoothed) Max thickness 7.3% at 27.1% chord Max camber 4.1% at 45.4% chord Max Cl/Cd 64.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(ma409sm-il) MA409 (smoothed) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Michael Achterberg MA409 F1C class free flight airfoil (smoothed) Max thickness 6.7% at 23.8% chord Max camber 3.3% at 49.3% chord Max Cl/Cd 64.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe304-il) GOE 304 (FRIEDRICHSHAFEN G02) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 304 (Friedrichshafen G02) airfoil Max thickness 9% at 29.8% chord Max camber 6.3% at 39.8% chord Max Cl/Cd 64.1 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(psu94097-il) PSU 94-097 (AIAA 2001-2478) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Maughmer PSU 94-097 winglet airfoil Max thickness 9.7% at 32.3% chord Max camber 4% at 46.3% chord Max Cl/Cd 64.1 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
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