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.
(goe482-il) GOE 482 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Gottingen 482 airfoil Max thickness 16.5% at 29.6% chord Max camber 8.8% at 39.6% chord Max Cl/Cd 100.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(goe243-il) GOE 243 (MVA PR.3) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Gottingen 243 (MVA PR.3) airfoil Max thickness 19% at 29.3% chord Max camber 8.4% at 59.4% chord Max Cl/Cd 99.1 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(s1223-il) S1223 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Selig S1223 high lift low Reynolds number airfoil Max thickness 12.1% at 19.8% chord Max camber 8.1% at 49% chord Max Cl/Cd 98.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(jn153-il) JN-153 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Narramore JN153 airfoil Max thickness 17.6% at 28.2% chord Max camber 8.4% at 38.1% chord Max Cl/Cd 98.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(s1223-il) S1223 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Selig S1223 high lift low Reynolds number airfoil Max thickness 12.1% at 19.8% chord Max camber 8.1% at 49% chord Max Cl/Cd 97.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(goe421-il) GOE 421 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Gottingen 421 airfoil Max thickness 19% at 29.3% chord Max camber 8.1% at 49.3% chord Max Cl/Cd 96.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(goe241-il) GOE 241 (MVA PR.1) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Gottingen 241 (MVA PR.1) airfoil Max thickness 18.9% at 29.5% chord Max camber 8.4% at 49.5% chord Max Cl/Cd 94.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(goe244-il) GOE 244 (MVA PR.4) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Gottingen 244 (MVA PR.4) airfoil Max thickness 17.7% at 19.6% chord Max camber 10% at 49.6% chord Max Cl/Cd 92.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(goe440-il) GOE 440 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Gottingen 440 airfoil Max thickness 15.3% at 30% chord Max camber 9.7% at 40% chord Max Cl/Cd 92.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(goe241-il) GOE 241 (MVA PR.1) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Gottingen 241 (MVA PR.1) airfoil Max thickness 18.9% at 29.5% chord Max camber 8.4% at 49.5% chord Max Cl/Cd 91.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database |
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