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.
(a18sm-il) A18 (smoothed) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Archer A18 F1C free flight airfoil (smoothed) Max thickness 7.3% at 27.1% chord Max camber 3.8% at 49.3% chord Max Cl/Cd 63.7 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(a18-il) A18 (original) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Archer A18 F1C free flight airfoil(original) Max thickness 7.3% at 30% chord Max camber 3.9% at 45% chord Max Cl/Cd 63.6 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe225-il) GOE 225 (MVA H.35) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 225 (MVA H.35) airfoil Max thickness 12.8% at 19.7% chord Max camber 7.6% at 49.7% chord Max Cl/Cd 63.5 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(hq358-il) HQ 3.5/8 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Quabeck HQ 3.5/8 R/C sailplane airfoil Max thickness 8% at 35% chord Max camber 3.5% at 50% chord Max Cl/Cd 63.5 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe610bm-il) GOE 610-B MOD. AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 610-B MOD airfoil Max thickness 7.7% at 30% chord Max camber 5.5% at 40% chord Max Cl/Cd 63.5 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 63.4 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe63-il) GOE 63 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 63 airfoil Max thickness 8.3% at 19.9% chord Max camber 6.7% at 39.9% chord Max Cl/Cd 63.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe57-il) GOE 57 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 57 airfoil Max thickness 6.3% at 19.9% chord Max camber 5.1% at 39.9% chord Max Cl/Cd 63.3 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 63.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe362-il) GOE 362 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 362 airfoil Max thickness 6.6% at 20% chord Max camber 5.3% at 40% chord Max Cl/Cd 63.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
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