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.
(goe364-il) GOE 364 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 364 airfoil Max thickness 10.8% at 30% chord Max camber 6.5% at 30% chord Max Cl/Cd 104 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(ah6407-il) AH-6-40-7 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Althaus AH 6-407 airfoil Max thickness 6.9% at 20% chord Max camber 5.5% at 40% chord Max Cl/Cd 104 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(fx60126-il) WORTMANN FX 60-126 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 60-126 airfoil Max thickness 12.6% at 27.9% chord Max camber 3.6% at 56.5% chord Max Cl/Cd 104 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe359-il) GOE 359 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 359 airfoil Max thickness 7.8% at 30% chord Max camber 5.8% at 40% chord Max Cl/Cd 103.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe371-il) GOE 371 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 371 airfoil Max thickness 7% at 29.9% chord Max camber 4.6% at 39.9% chord Max Cl/Cd 103.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(ua2-180-il) UA(2)-180 (University of Alberta/Marsden) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | UA(2)-180 airfoil for ultralight category aircraft Max thickness 18.1% at 31.5% chord Max camber 7% at 36.6% chord Max Cl/Cd 103.9 at Re# 500,000 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 103.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(e854-il) EPPLER E854 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E854 propeller airfoil Max thickness 13.4% at 32.3% chord Max camber 3.3% at 55.7% chord Max Cl/Cd 103.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe379-il) GOE 379 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 379 airfoil Max thickness 6.5% at 30% chord Max camber 5.2% at 40% chord Max Cl/Cd 103.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe361-il) GOE 361 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 361 airfoil Max thickness 6.8% at 20% chord Max camber 5.5% at 40% chord Max Cl/Cd 103.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
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