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.
(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 116.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(s4061-il) S4061-096-84 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Selig S4061 low Reynolds number airfoil Max thickness 9.6% at 30.9% chord Max camber 3.3% at 44.7% chord Max Cl/Cd 116.6 at Re# 500,000 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 116.6 at Re# 500,000 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 116.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(raf32-il) RAF 32 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | RAF-32 airfoil Max thickness 12.7% at 30% chord Max camber 5% at 50% chord Max Cl/Cd 116.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe06k-il) GOE 6K AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 6K airfoil Max thickness 7.5% at 50% chord Max camber 3.1% at 50% chord Max Cl/Cd 116.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(hq308-il) HQ 3.0/8 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Quabeck HQ 3.0/8 R/C sailplane airfoil Max thickness 8% at 35% chord Max camber 3% at 50% chord Max Cl/Cd 116.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe07k-il) GOE 7K AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 7K airfoil Max thickness 11% at 50% chord Max camber 4.5% at 50% chord Max Cl/Cd 116.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(stcyr24-il) St. CYR 24 (Bartel 35-IIIC) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | St. CYR 24 (Bartel 35-IIIC) airfoil Max thickness 12.4% at 30% chord Max camber 5.9% at 40% chord Max Cl/Cd 116.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe412-il) GOE 412 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 412 airfoil Max thickness 13.1% at 29.7% chord Max camber 5.1% at 39.7% chord Max Cl/Cd 116.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
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