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.

(l1003-il) LIEBECK L1003 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Liebeck high lift airfoil Max thickness 17.7% at 30% chord Max camber 6.5% at 30% chord Max Cl/Cd 10.1 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(fx77w258-il) WORTMANN FX 77-W-258 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 77-W-258 wind turbine airfoil Max thickness 26.1% at 30.9% chord Max camber 4.3% at 27.9% chord Max Cl/Cd 9.5 at Re# 200,000 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 8.8 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(fx79w660a-il) FX 79-W-660A		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortman FX 79-W-660A airfoil for use on wind turbines (W) Max thickness 66.4% at 46.7% chord Max camber 2.3% at 17% chord Max Cl/Cd 8.7 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(e863-il) EPPLER 863 STRUT AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E863 strut airfoil Max thickness 35.7% at 28.5% chord Max camber 0% at 0% chord Max Cl/Cd 8.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database

(goe570-il) GOE 570 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 570 airfoil Max thickness 33.7% at 30% chord Max camber 9.7% at 40% chord Max Cl/Cd 7.8 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(e864-il) EPPLER 864 STRUT AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E864 strut airfoil Max thickness 38.8% at 32.7% chord Max camber 0.1% at 10.8% chord Max Cl/Cd 7.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(fx79w660a-il) FX 79-W-660A		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortman FX 79-W-660A airfoil for use on wind turbines (W) Max thickness 66.4% at 46.7% chord Max camber 2.3% at 17% chord Max Cl/Cd 6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(chen-il) CHEN AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	University of Illinois at Urbana-Champaign / Chen high lift airfoil Max thickness 12.5% at 27.7% chord Max camber 7.8% at 25.4% chord Max Cl/Cd 5.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(ua79sff-il) UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	University of Alberta/Marsden UA 79-SF-187 sailplane airfoil FLAP Max thickness 8.7% at 73.1% chord Max camber 3.4% at 78.1% chord Max Cl/Cd 5.1 at Re# 200,000 Source UIUC Airfoil Coordinates Database