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.

(e561-il) EPPLER 561 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E561 general aviation airfoil Max thickness 16.9% at 27.9% chord Max camber 5.1% at 45.8% chord Max Cl/Cd 134.4 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe426-il) GOE 426 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 426 airfoil Max thickness 13.6% at 30% chord Max camber 4.6% at 40% chord Max Cl/Cd 134.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe456-il) GOE 456 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 456 airfoil Max thickness 7.2% at 29.9% chord Max camber 5.2% at 39.9% chord Max Cl/Cd 134.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e420-il) EPPLER 420 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E420 high lift airfoil Max thickness 14.3% at 22.8% chord Max camber 10.6% at 40.5% chord Max Cl/Cd 134.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe118-il) GOE 118 (MVA MK.7) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 118 (MVA MK.7) airfoil Max thickness 8.6% at 29.9% chord Max camber 5.7% at 39.9% chord Max Cl/Cd 134.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database

(e392-il) E392 (10.15%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E392 low Reynolds number airfoil Max thickness 10.1% at 31.6% chord Max camber 3.7% at 45.3% chord Max Cl/Cd 134 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e584-il) EPPLER 584 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E584 sailplane airfoil Max thickness 16.6% at 38.3% chord Max camber 4.5% at 38.3% chord Max Cl/Cd 134 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(mh38-il) MH 38 9.68%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 38 for Endurance Model Max thickness 9.7% at 31.6% chord Max camber 3.9% at 45.3% chord Max Cl/Cd 133.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(s4180-il) S4180-098-84		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig S4180 low Reynolds number airfoil Max thickness 9.8% at 26.1% chord Max camber 4% at 39.4% chord Max Cl/Cd 133.9 at Re# 1,000,000 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 133.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database