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.

(fx76mp160-il) FX 76-MP-160		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 76-MP-160 airfoil Max thickness 16.1% at 33.9% chord Max camber 6.1% at 50% chord Max Cl/Cd 72 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(mh117-il) MH 117 9.8%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 117 for a propeller for ultralight (tip) Max thickness 9.8% at 29.1% chord Max camber 2.7% at 44.6% chord Max Cl/Cd 72 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe199-il) GOE 199 (L.F.G. 5406) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 199 (L.F.G. 5406) airfoil Max thickness 7.3% at 30% chord Max camber 5.2% at 30% chord Max Cl/Cd 72 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(naca747a315-il) NACA 747A315		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 747A315 airfoil Max thickness 15% at 40.2% chord Max camber 2.5% at 35% chord Max Cl/Cd 72 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(e407-il) EPPLER 407 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E407 sailplane airfoil Max thickness 14.4% at 36.6% chord Max camber 3.5% at 71.7% chord Max Cl/Cd 72 at Re# 200,000 Source UIUC Airfoil Coordinates Database

(goe433-il) GOE 433 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 433 airfoil Max thickness 17.4% at 29.2% chord Max camber 4.8% at 49.2% chord Max Cl/Cd 71.9 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe685-il) GOE 685 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 685 airfoil Max thickness 13.1% at 19.6% chord Max camber 4.2% at 49.5% chord Max Cl/Cd 71.9 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(fx77w121-il) FX 77-W-121		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 77-W-121 airfoil for use on wind turbines (W) Max thickness 12.1% at 30.9% chord Max camber 4.6% at 30.9% chord Max Cl/Cd 71.9 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(fx61147-il) FX 61-147 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 61-147 airfoil Max thickness 14.8% at 33.9% chord Max camber 3.2% at 33.9% chord Max Cl/Cd 71.9 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe387-il) GOE 387 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 387 airfoil Max thickness 14.9% at 30% chord Max camber 5.5% at 40% chord Max Cl/Cd 71.9 at Re# 200,000 Source UIUC Airfoil Coordinates Database