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.

(goe279-il) GOE 279 (DAIMLER X) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 279 (DAIMLER X) airfoil Max thickness 7.4% at 30% chord Max camber 4.7% at 40% chord Max Cl/Cd 105 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe373-il) GOE 373 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 373 airfoil Max thickness 6.5% at 29.9% chord Max camber 5.1% at 39.9% chord Max Cl/Cd 105 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(raf6-il) RAF 6 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	RAF-6 airfoil Max thickness 10% at 30% chord Max camber 4.6% at 30% chord Max Cl/Cd 105 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e1230-il) EPPLER 1230 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E1230 general aviation airfoil (Long-EZ and Defiant wing airfoil) Max thickness 17.4% at 30.9% chord Max camber 3.6% at 25.6% chord Max Cl/Cd 104.9 at Re# 1,000,000 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 104.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database

(goe477-il) GOE 477 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 477 airfoil Max thickness 10.1% at 30% chord Max camber 4.9% at 40% chord Max Cl/Cd 104.9 at Re# 1,000,000 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 104.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e1233-il) EPPLER 1233 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E1233 general aviation airfoil Max thickness 18.9% at 29.8% chord Max camber 4.4% at 29.8% chord Max Cl/Cd 104.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe602-il) GOE 602 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 602 airfoil Max thickness 10% at 30% chord Max camber 3.5% at 40% chord Max Cl/Cd 104.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(usa34-il) USA 34 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	USA-34 airfoil Max thickness 18% at 29.5% chord Max camber 7.7% at 39.5% chord Max Cl/Cd 104.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database