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.
(goe652-il) GOE 652 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 652 airfoil Max thickness 17.1% at 20% chord Max camber 9.3% at 50% chord Max Cl/Cd 102.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe184-il) GOE 184 (MVA H.29) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 184 (MVA H.29) airfoil Max thickness 8.3% at 19.9% chord Max camber 5.3% at 39.9% chord Max Cl/Cd 102.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(a18sm-il) A18 (smoothed) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Archer A18 F1C free flight airfoil (smoothed) Max thickness 7.3% at 27.1% chord Max camber 3.8% at 49.3% chord Max Cl/Cd 102.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe433-il) GOE 433 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 433 airfoil Max thickness 17.4% at 29.2% chord Max camber 4.8% at 49.2% chord Max Cl/Cd 102.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(clarkk-il) CLARK K AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | CLARK K airfoil Max thickness 11.7% at 29.7% chord Max camber 3.3% at 39.6% chord Max Cl/Cd 102.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(m23-il) NACA M23 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA/Munk M-23 airfoil Max thickness 8.1% at 30.1% chord Max camber 6.4% at 30.1% chord Max Cl/Cd 102.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(e207-il) E207 (12.04%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E207 low Reynolds number airfoil Max thickness 12% at 29.6% chord Max camber 2.5% at 38.6% chord Max Cl/Cd 102.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe226-il) GOE 226 (MVA H.36) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 226 (MVA H.36) airfoil Max thickness 13.9% at 19.7% chord Max camber 8.1% at 49.7% chord Max Cl/Cd 102.7 at Re# 500,000 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 102.6 at Re# 500,000 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 102.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
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