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.
(naca652415-il) NACA 65(2)-415 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA 65(2)-415 airfoil Max thickness 15% at 39.9% chord Max camber 2.2% at 50% chord Max Cl/Cd 120.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(naca642415-il) NACA 64(2)-415 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA 64(2)-415 airfoil Max thickness 15% at 34.9% chord Max camber 2.2% at 50% chord Max Cl/Cd 120.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(ah93157-il) AH 93-157 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Althaus AH 93-157 airfoil Max thickness 15.7% at 39.6% chord Max camber 3.5% at 41.7% chord Max Cl/Cd 120.6 at Re# 1,000,000 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 120.6 at Re# 1,000,000 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 120.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe392-il) GOE 392 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 392 airfoil Max thickness 10.2% at 30% chord Max camber 4.8% at 40% chord Max Cl/Cd 120.6 at Re# 1,000,000 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 120.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe118-il) GOE 118 (MVA MK.7) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 118 (MVA MK.7) airfoil Max thickness 8.6% at 29.9% chord Max camber 5.7% at 39.9% chord Max Cl/Cd 120.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe623-il) GOE 623 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 623 airfoil Max thickness 12% at 30% chord Max camber 3.8% at 40% chord Max Cl/Cd 120.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e558-il) EPPLER 558 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E558 general aviation airfoil Max thickness 16% at 26.4% chord Max camber 3.8% at 49.3% chord Max Cl/Cd 120.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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