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.

(s8052-il) S8052 (11.88%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig S8052 low Reynolds number airfoil Max thickness 11.9% at 33.3% chord Max camber 1.2% at 44.2% chord Source UIUC Airfoil Coordinates Database
(naca651212-il) NACA 65(1)-212		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 65(1)-212 airfoil Max thickness 12% at 40% chord Max camber 1.1% at 50% chord Source UIUC Airfoil Coordinates Database
(hq1012-il) HQ 1.0/12 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Quabeck HQ 1.0/12 R/C sailplane airfoil Max thickness 12% at 35% chord Max camber 1% at 50% chord Source UIUC Airfoil Coordinates Database
(n63012a-il) NACA 63012A AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 63-012A airfoil Max thickness 12% at 35% chord Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database
(naca4412-il) NACA 4412		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 4412 airfoil Max thickness 12% at 30% chord Max camber 4% at 40% chord Source UIUC Airfoil Coordinates Database
(sc20412-il) NASA SC(2)-0412 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NASA SC(2)-0412 airfoil (NASA TP-2969) Max thickness 12% at 37% chord Max camber 1.3% at 83% chord Source UIUC Airfoil Coordinates Database
(eh2012-il) EH 2.0/12		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	John Yost EH 2.0/12 for tailless R/C aircraft Max thickness 12% at 28.7% chord Max camber 2% at 25.9% chord Source UIUC Airfoil Coordinates Database
(nacam18-il) NACA M18		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA M18 airfoil Max thickness 12% at 30% chord Max camber 4.1% at 30% chord Source UIUC Airfoil Coordinates Database
(goe767-il) GOE 767 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 767 airfoil Max thickness 12% at 20% chord Max camber 1.5% at 20% chord Source UIUC Airfoil Coordinates Database
(goe766-il) GOE 766 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 766 airfoil Max thickness 12% at 25% chord Max camber 1.5% at 20% chord Source UIUC Airfoil Coordinates Database

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