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.

(ah82150f-il) AH 82-150 F		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 82-150 F airfoil Max thickness 15% at 43.5% chord Max camber 3.6% at 46.7% chord Source UIUC Airfoil Coordinates Database
(goe693-il) GOE 693 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 693 airfoil Max thickness 12% at 30% chord Max camber 3.6% at 40% chord Source UIUC Airfoil Coordinates Database
(ah93w480b-il) AH 93-W-480B		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 93-W-480B airfoil for use on wind turbines (W) Max thickness 47.8% at 44.1% chord Max camber 3.6% at 44.1% chord Source UIUC Airfoil Coordinates Database
(n10-il) N-10		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	N-10 airfoil Max thickness 11.2% at 30% chord Max camber 3.6% at 40% chord Source UIUC Airfoil Coordinates Database
(e603-il) EPPLER 603 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E603 general purpose airfoil Max thickness 19% at 40% chord Max camber 3.6% at 35.6% chord Source UIUC Airfoil Coordinates Database

(isa571-il) I.S.A. 571		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	I.S.A. 571 airfoil Max thickness 7.4% at 30% chord Max camber 3.6% at 30% chord Source UIUC Airfoil Coordinates Database
(e637-il) EPPLER 637 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E637 airfoil Max thickness 12.1% at 27.6% chord Max camber 3.6% at 23.6% chord Source UIUC Airfoil Coordinates Database
(goe796-il) GOE 796 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 796 airfoil Max thickness 12% at 30% chord Max camber 3.6% at 40% chord Source UIUC Airfoil Coordinates Database
(sd7034-il) SD7034		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig/Donovan SD7034 low Reynolds number airfoil Max thickness 10.5% at 26% chord Max camber 3.6% at 39.4% chord Source UIUC Airfoil Coordinates Database
(oaf102-il) OAF102 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	ONERA/Aerospatiale OAF102 Fenestron airfoil Max thickness 10.2% at 28.7% chord Max camber 3.6% at 53.1% chord Source UIUC Airfoil Coordinates Database