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.
(goe432-il) GOE 432 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 432 airfoil Max thickness 7.7% at 20% chord Max camber 4.3% at 40% chord Max Cl/Cd 108 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(rhodesg32-il) Rhode St. Genese 32 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Rhode St. Genese 32 airfoil Max thickness 11.9% at 30% chord Max camber 3.9% at 40% chord Max Cl/Cd 108 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(clarkx-il) CLARK X AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | CLARK X airfoil Max thickness 11.7% at 30% chord Max camber 3.3% at 40% chord Max Cl/Cd 107.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(boe103-il) BOEING 103 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Boeing 103 airfoil Max thickness 12.7% at 30% chord Max camber 3.6% at 40% chord Max Cl/Cd 107.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe243-il) GOE 243 (MVA PR.3) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 243 (MVA PR.3) airfoil Max thickness 19% at 29.3% chord Max camber 8.4% at 59.4% chord Max Cl/Cd 107.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e332-il) EPPLER 332 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E332 flying wing airfoil Max thickness 11.5% at 32.3% chord Max camber 3.1% at 22.6% chord Max Cl/Cd 107.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe769-il) GOE 769 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 769 airfoil Max thickness 13.8% at 20% chord Max camber 4.8% at 30% chord Max Cl/Cd 107.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe611-il) GOE 611 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 611 airfoil Max thickness 12.9% at 29.9% chord Max camber 5.8% at 39.9% chord Max Cl/Cd 107.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe403-il) GOE 403 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 403 airfoil Max thickness 6.7% at 29.9% chord Max camber 4.3% at 39.9% chord Max Cl/Cd 107.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(eh3012-il) EH 3.0/12 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | John Yost EH 3.0/12 for tailless R/C aircraft Max thickness 12% at 30% chord Max camber 2.9% at 25% chord Max Cl/Cd 107.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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