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.

(coanda1-il) Coanda 1		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Coanda 1 airfoil Max thickness 5.7% at 30% chord Max camber 2.9% at 40% chord Source UIUC Airfoil Coordinates Database
(e61-il) E61 (5.64%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E61 low Reynolds number airfoil Max thickness 5.7% at 23.8% chord Max camber 6.4% at 51% chord Source UIUC Airfoil Coordinates Database
(goe346-il) GOE 346 (FRIEDRICHSHAFEN-STAAKEN) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 346 (Friedrichshafen-Staaken) airfoil Max thickness 5.7% at 39.9% chord Max camber 3.8% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe590-il) GOE 590 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 590 airfoil Max thickness 5.7% at 30% chord Max camber 4% at 30% chord Source UIUC Airfoil Coordinates Database
(ag08-il) AG08		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Drela AG08 airfoil Max thickness 5.8% at 21% chord Max camber 1.7% at 40.4% chord Source UIUC Airfoil Coordinates Database
(ag11-il) AG11		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Drela AG11 airfoil Max thickness 5.8% at 26% chord Max camber 2.2% at 29.7% chord Source UIUC Airfoil Coordinates Database
(ag13-il) AG13		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Drela AG13 airfoil Max thickness 5.8% at 21.3% chord Max camber 2% at 41.8% chord Source UIUC Airfoil Coordinates Database
(goe587-il) GOE 587 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 587 airfoil Max thickness 5.8% at 40% chord Max camber 3% at 30% chord Source UIUC Airfoil Coordinates Database
(ag18-il) AG18		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Drela AG18 airfoil Max thickness 5.9% at 20.7% chord Max camber 2.2% at 44.1% chord Source UIUC Airfoil Coordinates Database
(ah7476-il) AH-7-47-6 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 7-476 airfoil Max thickness 5.9% at 20% chord Max camber 6.2% at 50% chord Source UIUC Airfoil Coordinates Database

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