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.
(s9037-il) S9037 (9%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Selig S9037 (9%) low Reynolds number airfoil used on the Opus R/C sailplane Max thickness 9% at 28.5% chord Max camber 3.3% at 42.4% chord Max Cl/Cd 74.3 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(naca643618-il) NACA 64(3)-618 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA 64(3)-618 airfoil Max thickness 17.9% at 34.7% chord Max camber 3.3% at 50% chord Max Cl/Cd 74.3 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(goe308-il) GOE 308 (MVA H.40) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 308 (MVA H.40) airfoil Max thickness 8.1% at 29.9% chord Max camber 5% at 29.9% chord Max Cl/Cd 74.3 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(goe523-il) GOE 523 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 523 airfoil Max thickness 16.5% at 29.7% chord Max camber 9.7% at 49.7% chord Max Cl/Cd 74.3 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(goe525-il) GOE 525 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 525 airfoil Max thickness 16.5% at 29.7% chord Max camber 9.7% at 49.7% chord Max Cl/Cd 74.3 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(hq209-il) HQ 2.0/9 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Quabeck HQ 2.0/9 R/C sailplane airfoil Max thickness 9% at 35% chord Max camber 2% at 50% chord Max Cl/Cd 74.2 at Re# 200,000 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 74.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(e593-il) EPPLER 593 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E593 airfoil Max thickness 11.3% at 24.2% chord Max camber 4.6% at 29.2% chord Max Cl/Cd 74.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(goe190-il) GOE 190 (MVA MK.18) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 190 (MVA MK.18) airfoil Max thickness 12.7% at 19.7% chord Max camber 5.9% at 49.7% chord Max Cl/Cd 74.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
(goe548-il) GOE 548 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 548 airfoil Max thickness 11.9% at 40% chord Max camber 2.3% at 50% chord Max Cl/Cd 74.2 at Re# 200,000 Source UIUC Airfoil Coordinates Database | |
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