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.
(geminism-il) GEMINI (smoothed) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | GEMINI R/C sailplane airfoil (smoothed) Max thickness 15.4% at 34.2% chord Max camber 2.2% at 37.9% chord Max Cl/Cd 47.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(tempest2-il) HAWKER TEMPEST 61% SEMISPAN AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Hawker Tempest 61% semispan airfoil (NPL?) Max thickness 12% at 37.3% chord Max camber 0.9% at 39.3% chord Max Cl/Cd 47.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(m18-il) NACA M18 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | NACA/Munk M-18 airfoil Max thickness 12% at 30% chord Max camber 4.1% at 30% chord Max Cl/Cd 47.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe416a-il) GOE 416A AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 416A airfoil Max thickness 11.7% at 29.5% chord Max camber 1.3% at 59.6% chord Max Cl/Cd 47.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(naca001034a08cli02-il) NACA 0010-34 a=0.8 c(li)=0.2 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | NACA 0010-34 a=0.8 c(li)=0.2 airfoil Max thickness 10% at 40% chord Max camber 1.3% at 50% chord Max Cl/Cd 47.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(rg12-il) RG-12 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Rolf Girsberger RG 12 airfoil Max thickness 9.3% at 34.4% chord Max camber 1.4% at 34.4% chord Max Cl/Cd 47.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(e817-il) EPPLER 817 HYDROFOIL AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Eppler E817 hydrofoil Max thickness 11% at 32.9% chord Max camber 2.9% at 66.7% chord Max Cl/Cd 47.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe255-il) GOE 255 (MVA CA.6) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 255 (MVA CA.6) airfoil Max thickness 18.5% at 29.1% chord Max camber 4.8% at 49.1% chord Max Cl/Cd 47.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(rc12n1-il) NASA/LANGLEY RC-12(N)1 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | NASA/Langley RC-12(N)1 rotorcraft airfoil Max thickness 12% at 37.4% chord Max camber 1.4% at 30% chord Max Cl/Cd 47.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database | |
(goe344-il) GOE 344 (PFALZ 71) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
![]() | Gottingen 344 (Pfalz 71) airfoil Max thickness 7.2% at 19.9% chord Max camber 2.7% at 39.9% chord Max Cl/Cd 47.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database |
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