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.

(goe285-il) GOE 285 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 285 airfoil Max thickness 11.7% at 30% chord Max camber 3.7% at 30% chord Source UIUC Airfoil Coordinates Database
(goe416a-il) GOE 416A AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 416A airfoil Max thickness 11.7% at 29.5% chord Max camber 1.3% at 59.6% chord Source UIUC Airfoil Coordinates Database
(clarkz-il) CLARK Z AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	CLARK Z airfoil Max thickness 11.8% at 30% chord Max camber 4% at 40% chord Source UIUC Airfoil Coordinates Database
(e195-il) E195 (11.82%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E195 low Reynolds number airfoil Max thickness 11.8% at 35% chord Max camber 2.7% at 44.2% chord Source UIUC Airfoil Coordinates Database
(fx68h120-il) FX 68-H-120		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 68-H-120 airfoil Max thickness 11.8% at 25% chord Max camber 2.3% at 33.9% chord Source UIUC Airfoil Coordinates Database
(joukowsk-il) 12% JOUKOWSKI AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	12% Joukowski airfoil Max thickness 11.8% at 25% chord Max camber 0% at 9.5% chord Source UIUC Airfoil Coordinates Database
(n13-il) N-13		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	N-13 airfoil Max thickness 11.8% at 30% chord Max camber 0.1% at 95% chord Source UIUC Airfoil Coordinates Database
(fx082512-il) WORTMANN FX 082-512 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 082-512 airfoil Max thickness 11.8% at 25% chord Max camber 4.2% at 62.9% chord Source UIUC Airfoil Coordinates Database
(goe480-il) GOE 480 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 480 airfoil Max thickness 11.8% at 30% chord Max camber 5.5% at 40% chord Source UIUC Airfoil Coordinates Database
(goe431-il) GOE 431 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 431 airfoil Max thickness 11.8% at 20% chord Max camber 7.2% at 60% chord Source UIUC Airfoil Coordinates Database

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