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.

(goe601-il) GOE 601 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 601 airfoil Max thickness 16% at 39% chord Max camber 2.5% at 49% chord Source UIUC Airfoil Coordinates Database
(goe602-il) GOE 602 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 602 airfoil Max thickness 10% at 30% chord Max camber 3.5% at 40% chord Source UIUC Airfoil Coordinates Database
(goe602m-il) GOE 602 MOD. AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 602 MOD airfoil Max thickness 9.6% at 30% chord Max camber 3.8% at 50% chord Source UIUC Airfoil Coordinates Database
(goe604-il) GOE 604 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 604 airfoil Max thickness 17.8% at 29.3% chord Max camber 5.4% at 29.3% chord Source UIUC Airfoil Coordinates Database
(goe610b-il) GOE 610 B AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 610 B airfoil Max thickness 7.8% at 39.9% chord Max camber 5.3% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe610bm-il) GOE 610-B MOD. AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 610-B MOD airfoil Max thickness 7.7% at 30% chord Max camber 5.5% at 40% chord Source UIUC Airfoil Coordinates Database
(goe611-il) GOE 611 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 611 airfoil Max thickness 12.9% at 29.9% chord Max camber 5.8% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe612-il) GOE 612 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 612 airfoil Max thickness 15% at 29.5% chord Max camber 5% at 49.5% chord Source UIUC Airfoil Coordinates Database
(goe613-il) GOE 613 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 613 airfoil Max thickness 10.3% at 30% chord Max camber 4.1% at 40% chord Source UIUC Airfoil Coordinates Database
(goe614-il) GOE 614 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 614 airfoil Max thickness 18.8% at 29.2% chord Max camber 6.2% at 39.2% chord Source UIUC Airfoil Coordinates Database

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