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.
(fx77w153-il) WORTMANN FX 77-W-153 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Wortmann FX 77-W-153 wind turbine airfoil Max thickness 15.2% at 27.9% chord Max camber 4.5% at 27.9% chord Max Cl/Cd 33.8 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(dfvlrr4-il) DFVLR R-4 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | DFVLR R-4 transonic airfoil Max thickness 13.4% at 37.9% chord Max camber 2.1% at 79.9% chord Max Cl/Cd 33.8 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe625-il) GOE 625 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 625 airfoil Max thickness 20% at 30% chord Max camber 6.1% at 40% chord Max Cl/Cd 33.8 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(mh92-il) MH 92 15.49% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Martin Hepperle MH 92 parafoil Max thickness 15.5% at 27.4% chord Max camber 1.4% at 15.1% chord Max Cl/Cd 33.8 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(s9026-il) S9026 (9.5%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Selig S9026 (9.5%) symmetrical horizontal stab airfoil used on the Opus R/C sailplane Max thickness 9.5% at 27.3% chord Max camber 0% at 0% chord Max Cl/Cd 33.8 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(sc20710-il) NASA SC(2)-0710 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | NASA SC(2)-0710 airfoil (NASA TP-2969) Max thickness 10% at 37% chord Max camber 2.1% at 81% chord Max Cl/Cd 33.8 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(e338-il) EPPLER 338 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E338 flying wing airfoil Max thickness 13.3% at 31.1% chord Max camber 3.7% at 26.2% chord Max Cl/Cd 33.8 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(saratov-il) SARATOV AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Saratov R/C sailplane airfoil Max thickness 9.2% at 15% chord Max camber 9.8% at 40% chord Max Cl/Cd 33.7 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(rcsc2-il) NASA/LANGLEY RC-SC2 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | NASA/Langley RC-SC2 rotorcraft airfoil Max thickness 10% at 40% chord Max camber 0.5% at 62.5% chord Max Cl/Cd 33.7 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(naca23015-il) NACA 23015 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | NACA 23015 airfoil Max thickness 15% at 30% chord Max camber 1.8% at 15% chord Max Cl/Cd 33.7 at Re# 100,000 Source UIUC Airfoil Coordinates Database |
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