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.

(fx79w660a-il) FX 79-W-660A		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortman FX 79-W-660A airfoil for use on wind turbines (W) Max thickness 66.4% at 46.7% chord Max camber 2.3% at 17% chord Source UIUC Airfoil Coordinates Database
(ah93w480b-il) AH 93-W-480B		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 93-W-480B airfoil for use on wind turbines (W) Max thickness 47.8% at 44.1% chord Max camber 3.6% at 44.1% chord Source UIUC Airfoil Coordinates Database
(fx79w470a-il) FX 79-W-470A		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 79-W-470A airfoil for use on wind turbines (W) Max thickness 46.4% at 37.1% chord Max camber 3.8% at 22.2% chord Source UIUC Airfoil Coordinates Database
(e864-il) EPPLER 864 STRUT AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E864 strut airfoil Max thickness 38.8% at 32.7% chord Max camber 0.1% at 10.8% chord Source UIUC Airfoil Coordinates Database
(e863-il) EPPLER 863 STRUT AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E863 strut airfoil Max thickness 35.7% at 28.5% chord Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database
(fx77w343-il) WORTMANN FX 77-W-343 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-343 wind turbine airfoil Max thickness 34.4% at 33.9% chord Max camber 4.7% at 25% chord Source UIUC Airfoil Coordinates Database
(goe570-il) GOE 570 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 570 airfoil Max thickness 33.7% at 30% chord Max camber 9.7% at 40% chord Source UIUC Airfoil Coordinates Database
(e862-il) EPPLER 862 STRUT AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E862 strut airfoil Max thickness 32.4% at 28.5% chord Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database
(griffith30symsuction-il) Griffith 30% Suction Airfoil		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Griffith 30% suction airfoil Max thickness 30.6% at 49.3% chord Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database
(ah94w301-il) AH 94-W-301		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 94-W-301 airfoil for use on wind turbines (W) Max thickness 30.1% at 30.9% chord Max camber 1.3% at 80.4% chord Source UIUC Airfoil Coordinates Database

Page 1 of 164     1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20     Next

Please see the source web site or designer for any license conditions.