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.

(s1016-il) S1016		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig S1016 HPV airfoil Max thickness 17.5% at 41.8% chord Max camber 0% at 0% chord Max Cl/Cd 39.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(naca001234-il) NACA 0012-34		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 0012-34 airfoil Max thickness 12% at 40% chord Max camber 0% at 0% chord Max Cl/Cd 39.2 at Re# 100,000 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 39.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(naca643418-il) NACA 64(3)-418		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 64(3)-418 airfoil Max thickness 17.9% at 34.8% chord Max camber 2.2% at 50% chord Max Cl/Cd 39.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(e325-il) EPPLER 325 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E325 flying wing airfoil Max thickness 12.6% at 34.3% chord Max camber 1.8% at 16.3% chord Max Cl/Cd 39.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database

(e625-il) EPPLER 625 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E625 airfoil Max thickness 13% at 30% chord Max camber 2.9% at 22.5% chord Max Cl/Cd 39.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(sc21006-il) NASA SC(2)-1006 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NASA SC(2)-1006 airfoil Max thickness 6% at 30% chord Max camber 2.6% at 73% chord Max Cl/Cd 39.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(goe518-il) GOE 518 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 518 airfoil Max thickness 18% at 29.8% chord Max camber 7.3% at 29.8% chord Max Cl/Cd 39.1 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(naca23015-il) NACA 23015		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 23015 airfoil Max thickness 15% at 30% chord Max camber 1.8% at 15% chord Max Cl/Cd 39.1 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(raf30-il) RAF 30 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	RAF-30 airfoil Max thickness 12.6% at 30% chord Max camber 0% at 0% chord Max Cl/Cd 39.1 at Re# 100,000 Source UIUC Airfoil Coordinates Database