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.

(s4022-il) S4022		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig S4022 low Reynolds number airfoil Max thickness 11.3% at 34.1% chord Max camber 4.3% at 57.8% chord Max Cl/Cd 113.5 at Re# 500,000 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 113.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e66-il) EPPLER 66 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E66 low Reynolds number airfoil Max thickness 10.1% at 28.7% chord Max camber 4.1% at 52.3% chord Max Cl/Cd 113.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e593-il) EPPLER 593 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E593 airfoil Max thickness 11.3% at 24.2% chord Max camber 4.6% at 29.2% chord Max Cl/Cd 113.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(fx66s171-il) FX 66-S-171 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 66-S-171 airfoil Max thickness 17.1% at 33.9% chord Max camber 3.9% at 43.5% chord Max Cl/Cd 113.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(fx057816-il) WORTMANN FX 057-816		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 057-816 airfoil Max thickness 16.2% at 37.1% chord Max camber 5.1% at 37.1% chord Max Cl/Cd 113.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(fx84w140-il) FX 84-W-140		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 84-W-140 airfoil for use on wind turbines (W) Max thickness 14.1% at 37.1% chord Max camber 4.2% at 40.2% chord Max Cl/Cd 113.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e715-il) EPPLER 715 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E715 tailplane airfoil Max thickness 15% at 33.1% chord Max camber 2.8% at 42% chord Max Cl/Cd 113.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(ah88k136-il) AH 88-K-136/16		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 88-K-136/16 airfoil for use with flaps (K) Max thickness 13.5% at 44.9% chord Max camber 3% at 41.9% chord Max Cl/Cd 113.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe501-il) GOE 501 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 501 airfoil Max thickness 12.8% at 30% chord Max camber 6.3% at 50% chord Max Cl/Cd 113.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database