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.
(e637-il) EPPLER 637 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E637 airfoil Max thickness 12.1% at 27.6% chord Max camber 3.6% at 23.6% chord Max Cl/Cd 117.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(vr5-il) BOEING-VERTOL VR-5 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Boeing-Vertol VR-5 rotorcraft airfoil Max thickness 12% at 35% chord Max camber 3.4% at 35% chord Max Cl/Cd 117.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe422-il) GOE 422 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 422 airfoil Max thickness 17.1% at 29.5% chord Max camber 6.5% at 39.5% chord Max Cl/Cd 117.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(mh150-il) MH 150 23.89% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Martin Hepperle MH 150 for marine ruddershaft for torque reduction (schottel units) Max thickness 23.9% at 27.2% chord Max camber 4.5% at 53.8% chord Max Cl/Cd 117.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe464-il) GOE 464 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 464 airfoil Max thickness 7.7% at 7.4% chord Max camber 9.9% at 29.9% chord Max Cl/Cd 117.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe509-il) GOE 509 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 509 airfoil Max thickness 11.1% at 29.9% chord Max camber 5.2% at 39.9% chord Max Cl/Cd 117.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(august160-il) AUGUST 160 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | AUGUST 160 airfoil Max thickness 16% at 25% chord Max camber 5.4% at 25% chord Max Cl/Cd 117.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe702-il) GOE 702 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 702 airfoil Max thickness 16.6% at 19.4% chord Max camber 5.1% at 39.4% chord Max Cl/Cd 117.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e548-il) EPPLER 548 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E548 general aviation airfoil Max thickness 17.4% at 35.4% chord Max camber 2.2% at 26.1% chord Max Cl/Cd 117.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe304-il) GOE 304 (FRIEDRICHSHAFEN G02) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 304 (Friedrichshafen G02) airfoil Max thickness 9% at 29.8% chord Max camber 6.3% at 39.8% chord Max Cl/Cd 117.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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