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.
(hq259-il) HQ 2.5/9 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Quabeck HQ 2.5/9 R/C sailplane airfoil Max thickness 9% at 35% chord Max camber 2.5% at 50% chord Max Cl/Cd 122 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe08k-il) GOE 8K AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 8K airfoil Max thickness 14.9% at 50% chord Max camber 6.1% at 50% chord Max Cl/Cd 122 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(naca654421-il) NACA 65(4)-421 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA 65(4)-421 airfoil Max thickness 21% at 39.9% chord Max camber 2.2% at 50% chord Max Cl/Cd 122 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe330-il) GOE 330 (PFALZ 59) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 330 (Pfalz 59) airfoil Max thickness 10.2% at 29.9% chord Max camber 5.8% at 39.9% chord Max Cl/Cd 121.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(m14-il) NACA M14 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA/Munk M-14 airfoil Max thickness 8.1% at 30% chord Max camber 3.9% at 30% chord Max Cl/Cd 121.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe483-il) GOE 483 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 483 airfoil Max thickness 5.5% at 15% chord Max camber 5.8% at 40% chord Max Cl/Cd 121.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe369-il) GOE 369 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 369 airfoil Max thickness 5.9% at 30% chord Max camber 5.4% at 40% chord Max Cl/Cd 121.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe574-il) GOE 574 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 574 airfoil Max thickness 10.3% at 30% chord Max camber 4.9% at 40% chord Max Cl/Cd 121.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe264-il) GOE 264 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 264 airfoil Max thickness 6.4% at 20.2% chord Max camber 5.7% at 28.9% chord Max Cl/Cd 121.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(raf48-il) RAF-48 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | RAF-48 airfoil Max thickness 15% at 30% chord Max camber 2.9% at 40% chord Max Cl/Cd 121.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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