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.

(fx66s171-il) FX 66-S-171 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 66-S-171 airfoil Max thickness 17.1% at 33.9% chord Max camber 3.9% at 43.5% chord Max Cl/Cd 13.3 at Re# 100,000 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 13.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(r1046-il) RONCZ 1046 VOYAGER CANARD AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Roncz 1046 Voyager canard airfoil Max thickness 18.1% at 38% chord Max camber 6.7% at 42% chord Max Cl/Cd 13 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(fx77w270-il) FX 77-W-270		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 77-W-270 airfoil for use on wind turbines (W) Max thickness 27.1% at 33.9% chord Max camber 4.3% at 27.9% chord Max Cl/Cd 12.8 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(s811-nr) NREL's S811 Airfoil		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source file
	NREL HAWT airfoil S811 root Max thickness 26.3% at 27.4% chord Max camber 1.7% at 76.4% chord Max Cl/Cd 12.8 at Re# 100,000 Source NWTC National WInd Technology Center

(fx66a175-il) WORTMANN FX 66-17A-175 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 66-17A-175 airfoil Max thickness 17.5% at 33.9% chord Max camber 4.2% at 40.2% chord Max Cl/Cd 12.6 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(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 12.5 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(th25816-il) TH 25816 HALE AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Naval Air Development Center/Doug Hall high altitude Max thickness 25.7% at 48.3% chord Max camber 4% at 52.9% chord Max Cl/Cd 12.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(goe448-il) GOE 448 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 448 airfoil Max thickness 12.9% at 29.8% chord Max camber 10.5% at 39.8% chord Max Cl/Cd 11.5 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(gu255118-il) UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	University of Glasgow GU 25-5(11)8 canard airfoil (Quickie Max thickness 20% at 40% chord Max camber 7.1% at 45% chord Max Cl/Cd 11.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database