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.

(goe276-il) GOE 276 (DAIMLER VII) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 276 (DAIMLER VII) airfoil Max thickness 7.3% at 30% chord Max camber 4% at 30% chord Max Cl/Cd 93.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(fg1-il) Fage & Collins 1		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Fage & Collins 1 airfoil Max thickness 8.2% at 30% chord Max camber 3.1% at 40% chord Max Cl/Cd 93.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(clarkz-il) CLARK Z AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	CLARK Z airfoil Max thickness 11.8% at 30% chord Max camber 4% at 40% chord Max Cl/Cd 93.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe546-il) GOE 546 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 546 airfoil Max thickness 10.4% at 30% chord Max camber 3.6% at 50% chord Max Cl/Cd 93.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(fx75193-il) WORTMANN FX 75-193		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 75-193 airfoil Max thickness 19.3% at 40.2% chord Max camber 3.7% at 69.1% chord Max Cl/Cd 93.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(goe615-il) GOE 615 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 615 airfoil Max thickness 13.7% at 29.7% chord Max camber 5.6% at 39.7% chord Max Cl/Cd 93.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(eiffel385-il) Eiffel 385 (S.T. Ae)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eiffel 385 (S.T. Ae) airfoil Max thickness 13.4% at 20% chord Max camber 4.4% at 50% chord Max Cl/Cd 93.5 at Re# 500,000 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 93.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe645-il) GOE 645 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 645 airfoil Max thickness 15.4% at 19.4% chord Max camber 4.8% at 39.4% chord Max Cl/Cd 93.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe457-il) GOE 457 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 457 airfoil Max thickness 7.8% at 19.9% chord Max camber 4.2% at 39.9% chord Max Cl/Cd 93.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database