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.

(goe617-il) GOE 617 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 617 airfoil Max thickness 13.9% at 30% chord Max camber 2.2% at 30% chord Max Cl/Cd 87.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(drgnfly-il) DRAGONFLY CANARD		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Dragonfly Canard airfoil Max thickness 19.3% at 37.6% chord Max camber 6.6% at 40.9% chord Max Cl/Cd 87.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(usa28-il) USA 28 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	USA-28 airfoil Max thickness 13.2% at 29.9% chord Max camber 3.8% at 49.9% chord Max Cl/Cd 87.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(psu-90-125wl-il) PSU-90-125WL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	PSU-90-125WL sailplane winglet airfoil Max thickness 12.5% at 35.1% chord Max camber 2% at 54.4% chord Max Cl/Cd 87.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e336-il) EPPLER 336 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E336 flying wing airfoil Max thickness 12.8% at 28.1% chord Max camber 2.8% at 23.4% chord Max Cl/Cd 87.8 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(goe604-il) GOE 604 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 604 airfoil Max thickness 17.8% at 29.3% chord Max camber 5.4% at 29.3% chord Max Cl/Cd 87.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(sd7084-il) SD7084 (9.6%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig/Donovan SD7084 low Reynolds number airfoil Max thickness 9.6% at 29.5% chord Max camber 2.3% at 38.9% chord Max Cl/Cd 87.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe449-il) GOE 449 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 449 airfoil Max thickness 17% at 30% chord Max camber 5.4% at 40% chord Max Cl/Cd 87.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e682-il) EPPLER 682 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E682 sailplane airfoil Max thickness 15.3% at 40.4% chord Max camber 2.9% at 40.4% chord Max Cl/Cd 87.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe770-il) GOE 770 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 770 airfoil Max thickness 21% at 30% chord Max camber 4% at 30% chord Max Cl/Cd 87.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database