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.
(mh43-il) MH 43 8.5% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Martin Hepperle MH 43 for F3B and F3E Max thickness 8.5% at 31.4% chord Max camber 1.7% at 36.4% chord Max Cl/Cd 86.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(usa27m2-il) USA 27 mod. AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | USA-27MOD airfoil Max thickness 13.3% at 30% chord Max camber 5% at 40% chord Max Cl/Cd 86.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe210-il) GOE 210 (DAIMLER) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 210 (DAIMLER) airfoil Max thickness 6.6% at 30% chord Max camber 4.3% at 40% chord Max Cl/Cd 86.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe595-il) GOE 595 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 595 airfoil Max thickness 9.6% at 30% chord Max camber 3% at 40% chord Max Cl/Cd 86.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe143-il) GOE 143 (MVA H.20) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 143 (MVA H.20) airfoil Max thickness 7.4% at 19.9% chord Max camber 3.8% at 29.9% chord Max Cl/Cd 86.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(hq3013-il) HQ 3.0/13 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Quabeck HQ 3.0/13 R/C sailplane airfoil Max thickness 13% at 35% chord Max camber 3% at 50% chord Max Cl/Cd 86.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe147-il) GOE 147 (MVA H.6) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 147 (MVA H.6) airfoil Max thickness 7.5% at 14.9% chord Max camber 3.8% at 29.9% chord Max Cl/Cd 86.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(goe113-il) GOE 113 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 113 airfoil Max thickness 6.7% at 30% chord Max camber 3% at 40% chord Max Cl/Cd 86.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(hq158-il) HQ 1.5/8 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Quabeck HQ 1.5/8 R/C sailplane airfoil Max thickness 8% at 32.5% chord Max camber 1.5% at 50% chord Max Cl/Cd 86.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database | |
(m12-il) NACA M12 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | NACA/Munk M-12 airfoil Max thickness 11.9% at 30% chord Max camber 2% at 30% chord Max Cl/Cd 86.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database |
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