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.

(goe632-il) GOE 632 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 632 airfoil Max thickness 14% at 30% chord Max camber 3.9% at 40% chord Max Cl/Cd 69.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe256-il) GOE 256 (JUNKERS E) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 256 (JUNKERS E) airfoil Max thickness 16% at 29.6% chord Max camber 4.7% at 39.6% chord Max Cl/Cd 69.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe600-il) GOE 600 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 600 airfoil Max thickness 13.1% at 29.4% chord Max camber 1.9% at 49.4% chord Max Cl/Cd 69.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(fx83w160-il) FX 83-W-160		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 83-W-160 airfoil for use on wind turbines (W) Max thickness 16.1% at 37.1% chord Max camber 3.9% at 62.9% chord Max Cl/Cd 69.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe508-il) GOE 508 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 508 airfoil Max thickness 16.5% at 30% chord Max camber 5.6% at 40% chord Max Cl/Cd 69.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database

(goe415-il) GOE 415 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 415 airfoil Max thickness 8.5% at 19.9% chord Max camber 3.7% at 29.9% chord Max Cl/Cd 69.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(usa26-il) USA 26 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	USA-26 airfoil Max thickness 9.8% at 19.9% chord Max camber 4.3% at 39.9% chord Max Cl/Cd 69.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(e1200-il) EPPLER 1200 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E1200 general aviation airfoil Max thickness 16.9% at 36.1% chord Max camber 3.5% at 50.2% chord Max Cl/Cd 69.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(sa7036-il) SA7036		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig / Ashok Gopalarathnam SA7036 Max thickness 9.2% at 28.1% chord Max camber 2.6% at 42.1% chord Max Cl/Cd 69.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(ste87391-il) EPPLER STE 87(-3)-914 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler STE 87(-3)-914 airfoil Max thickness 14.6% at 34.1% chord Max camber 4.2% at 58.3% chord Max Cl/Cd 69.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database