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.

(goe531-il) GOE 531 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 531 airfoil Max thickness 13.8% at 19.5% chord Max camber 14.7% at 49.3% chord Max Cl/Cd 7.7 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(strand-il) STRAND AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Strand high lift airfoil Max thickness 15.4% at 26.1% chord Max camber 4.1% at 32.1% chord Max Cl/Cd 7.5 at Re# 100,000 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 7.1 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(fx84w218-il) FX 84-W-218		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 84-W-218 airfoil for use on wind turbines (W) Max thickness 22% at 33.9% chord Max camber 3.2% at 43.5% chord Max Cl/Cd 7.1 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(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 7 at Re# 100,000 Source UIUC Airfoil Coordinates Database

(lnv109a-il) LNV109A		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Douglas/Liebeck LNV109A high lift airfoil Max thickness 13% at 23.5% chord Max camber 6% at 31.5% chord Max Cl/Cd 7 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(ah94w301-il) AH 94-W-301		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 94-W-301 airfoil for use on wind turbines (W) Max thickness 30.1% at 30.9% chord Max camber 1.3% at 80.4% chord Max Cl/Cd 6.6 at Re# 100,000 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 6.3 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(ah93w215-il) AH 93-W-215		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 93-W-215 airfoil for use on wind turbines (W) Max thickness 21.2% at 33.9% chord Max camber 3.1% at 40.2% chord Max Cl/Cd 6.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database
(fx049915-il) WORTMANN FX 049-915 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 049-915 airfoil Max thickness 14.7% at 37.1% chord Max camber 5.8% at 37.1% chord Max Cl/Cd 6.2 at Re# 100,000 Source UIUC Airfoil Coordinates Database