Airfoil Tools
Search 1638 airfoils

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Your Reynold number range is 50,000 to 1,000,000. (set)

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.

(m20-il) NACA M20 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA/Munk M-20 airfoil Max thickness 8.2% at 30% chord Max camber 6.1% at 30% chord Max Cl/Cd 10.4 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(fx049915-il) WORTMANN FX 049-915 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 049-915 airfoil Max thickness 14.7% at 37.1% chord Max camber 5.8% at 37.1% chord Max Cl/Cd 10.4 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe798-il) GOE 798 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 798 airfoil Max thickness 20% at 30% chord Max camber 6% at 40% chord Max Cl/Cd 10.4 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(fx72150a-il) WORTMANN FX 72-MS-150A AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 72-MS-150A airfoil Max thickness 15% at 37.1% chord Max camber 8.3% at 46.7% chord Max Cl/Cd 10.4 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe615-il) GOE 615 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 615 airfoil Max thickness 13.7% at 29.7% chord Max camber 5.6% at 39.7% chord Max Cl/Cd 10.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database

(fx84w175-il) FX 84-W-175		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 84-W-175 airfoil for use on wind turbines (W) Max thickness 17.6% at 37.1% chord Max camber 4.4% at 43.5% chord Max Cl/Cd 10.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe513-il) GOE 513 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 513 airfoil Max thickness 16.6% at 29.8% chord Max camber 5.2% at 39.8% chord Max Cl/Cd 10.3 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe480-il) GOE 480 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 480 airfoil Max thickness 11.8% at 30% chord Max camber 5.5% at 40% chord Max Cl/Cd 10.2 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(naca654421a05-il) NACA 65(4)-421 a=0.5		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 65(4)-421 a=0.5 airfoil Max thickness 21% at 39.9% chord Max camber 3% at 45% chord Max Cl/Cd 10.2 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(e603-il) EPPLER 603 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E603 general purpose airfoil Max thickness 19% at 40% chord Max camber 3.6% at 35.6% chord Max Cl/Cd 10.2 at Re# 50,000 Source UIUC Airfoil Coordinates Database