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.

(ec863914-il) EPPLER EC 86(-3)-914 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler EC 86(-3)-914 airfoil Max thickness 14.3% at 35.5% chord Max camber 4.4% at 71.2% chord Max Cl/Cd 150.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(mh116-il) MH 116 9.84%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 116 for a propeller for ultralight Max thickness 9.9% at 32.4% chord Max camber 4.1% at 46.4% chord Max Cl/Cd 150.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(fx74130wp2-il) 74-130 WP2		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann 74-130 WP2 airfoil Max thickness 13% at 43.5% chord Max camber 3.9% at 46.7% chord Max Cl/Cd 150.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(psu94097-il) PSU 94-097 (AIAA 2001-2478)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Maughmer PSU 94-097 winglet airfoil Max thickness 9.7% at 32.3% chord Max camber 4% at 46.3% chord Max Cl/Cd 150.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(s4158-il) S4158		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig S4158 low Reynolds number airfoil Max thickness 10.9% at 35.3% chord Max camber 3.7% at 44.7% chord Max Cl/Cd 150.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database

(e655-il) EPPLER 655 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E655 sailplane airfoil Max thickness 17.3% at 37.3% chord Max camber 3.9% at 42.4% chord Max Cl/Cd 150.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(n1h15-il) NACA 1-H-15 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 1-H-15 rotorcraft airfoil Max thickness 14.7% at 40% chord Max camber 5.5% at 40% chord Max Cl/Cd 150.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe496-il) GOE 496 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 496 airfoil Max thickness 10% at 30% chord Max camber 5% at 50% chord Max Cl/Cd 150.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(fx74modsm-il) FX 74-Cl5-140 MOD (smoothed)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Modified Wortmann FX 74-CL5-140 high lift airfoil Max thickness 13.1% at 27.1% chord Max camber 9.7% at 41.6% chord Max Cl/Cd 149.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(fx74cl5140-il) FX74_CL5_140		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 74-CL5-140 high lift airfoil Max thickness 14% at 30.9% chord Max camber 9.9% at 37.1% chord Max Cl/Cd 149.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database