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.

(e587-il) EPPLER 587 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E587 sailplane airfoil Max thickness 16.6% at 41.1% chord Max camber 4.2% at 51.2% chord Max Cl/Cd 131.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(fx74130wp2mod-il) 74-130 WP2 MOD		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann 74-130 WP2 MOD airfoil Max thickness 12.9% at 43.5% chord Max camber 3.9% at 43.5% chord Max Cl/Cd 131.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e580-il) EPPLER 580 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E580 general purpose airfoil Max thickness 16.1% at 33% chord Max camber 4.1% at 61.2% chord Max Cl/Cd 131.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe362-il) GOE 362 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 362 airfoil Max thickness 6.6% at 20% chord Max camber 5.3% at 40% chord Max Cl/Cd 131.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e266-il) EPPLER 266 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E266 general purpose airfoil Max thickness 17.3% at 39.8% chord Max camber 3.1% at 39.8% chord Max Cl/Cd 131.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database

(e585-il) EPPLER 585 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E585 sailplane airfoil Max thickness 14.6% at 37.6% chord Max camber 4.2% at 42.8% chord Max Cl/Cd 131.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(ah6407-il) AH-6-40-7 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 6-407 airfoil Max thickness 6.9% at 20% chord Max camber 5.5% at 40% chord Max Cl/Cd 131.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(fx83w160-il) FX 83-W-160		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 83-W-160 airfoil for use on wind turbines (W) Max thickness 16.1% at 37.1% chord Max camber 3.9% at 62.9% chord Max Cl/Cd 131.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe360-il) GOE 360 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 360 airfoil Max thickness 9.7% at 29.9% chord Max camber 5.9% at 29.9% chord Max Cl/Cd 131.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe332-il) GOE 332 (PFALZ 61) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 332 (Pfalz 61) airfoil Max thickness 11.8% at 29.8% chord Max camber 6.4% at 39.8% chord Max Cl/Cd 131.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database