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.

(e423-il) E423		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E423 high lift airfoil Max thickness 12.5% at 23.7% chord Max camber 9.5% at 41.4% chord Max Cl/Cd 123.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e399-il) EPPLER 399 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E399 human powered aircraft airfoil Max thickness 14.8% at 29% chord Max camber 5.1% at 51.4% chord Max Cl/Cd 123.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(fx72150a-il) WORTMANN FX 72-MS-150A AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 72-MS-150A airfoil Max thickness 15% at 37.1% chord Max camber 8.3% at 46.7% chord Max Cl/Cd 123.1 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e668-il) EPPLER 668 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E668 sailplane airfoil Max thickness 13.9% at 37.3% chord Max camber 4% at 47.8% chord Max Cl/Cd 123 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(miley-il) MILEY M06-13-128		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Miley MO6-13-128 airfoil Max thickness 12.9% at 35% chord Max camber 4.9% at 35% chord Max Cl/Cd 122.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(fx62k153-il) FX 62-K-153/20 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 62-K-153/20 airfoil Max thickness 15.3% at 40.2% chord Max camber 4.1% at 62.9% chord Max Cl/Cd 122.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe304-il) GOE 304 (FRIEDRICHSHAFEN G02) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 304 (Friedrichshafen G02) airfoil Max thickness 9% at 29.8% chord Max camber 6.3% at 39.8% chord Max Cl/Cd 122.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe495-il) GOE 495 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 495 airfoil Max thickness 6.9% at 30% chord Max camber 5% at 50% chord Max Cl/Cd 122.7 at Re# 500,000 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 122.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e654-il) EPPLER 654 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E654 sailplane airfoil Max thickness 17.2% at 36.1% chord Max camber 4.9% at 46.5% chord Max Cl/Cd 122.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database