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.
(e1098-il) EPPLER 1098 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Eppler E1098 general aviation airfoil Max thickness 18.9% at 36.6% chord Max camber 3.7% at 54.5% chord Max Cl/Cd 117.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(ah81k144-il) AH 81-K-144/17 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Althaus AH 81-K-144/17 airfoil for use with flaps (K) Max thickness 14.5% at 40.2% chord Max camber 4.2% at 46.7% chord Max Cl/Cd 117.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(s4320-il) S4320 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Selig S4320 low Reynolds number airfoil Max thickness 9.4% at 26.8% chord Max camber 4.5% at 40.2% chord Max Cl/Cd 117.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(fx72150b-il) WORTMANN FX 72-MS-150B AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Wortmann FX 72-MS-150B airfoil Max thickness 15% at 37.1% chord Max camber 9.7% at 46.7% chord Max Cl/Cd 117.1 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(goe238-il) GOE 238 (HANSA-BRANDENBURG) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Gottingen 238 (HANSA-BRANDENBURG) airfoil Max thickness 9.8% at 29.8% chord Max camber 5.5% at 29.8% chord Max Cl/Cd 117.1 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(fx67k170-il) FX 67-K-170/17 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Wortmann FX 67-K-170/17 airfoil Max thickness 17% at 40.2% chord Max camber 5.1% at 43.5% chord Max Cl/Cd 116.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(e655-il) EPPLER 655 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Eppler E655 sailplane airfoil Max thickness 17.3% at 37.3% chord Max camber 3.9% at 42.4% chord Max Cl/Cd 116.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(goe242-il) GOE 242 (MVA PR.2) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Gottingen 242 (MVA PR.2) airfoil Max thickness 16.2% at 29.6% chord Max camber 7.5% at 49.7% chord Max Cl/Cd 116.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(oaf095-il) OAF095 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
ONERA/Aerospatiale OAF095 Fenestron airfoil Max thickness 9.5% at 23.2% chord Max camber 3.9% at 53.1% chord Max Cl/Cd 116.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | ||
(e678-il) EPPLER 678 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
Eppler E678 sailplane airfoil Max thickness 15.1% at 39.8% chord Max camber 5.1% at 53.7% chord Max Cl/Cd 116.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database |
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