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.

(goe572-il) GOE 572 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 572 airfoil Max thickness 18.6% at 29.9% chord Max camber 8.3% at 29.9% chord Source UIUC Airfoil Coordinates Database
(goe573-il) GOE 573 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 573 airfoil Max thickness 14.1% at 29.9% chord Max camber 6.5% at 29.9% chord Source UIUC Airfoil Coordinates Database
(goe574-il) GOE 574 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 574 airfoil Max thickness 10.3% at 30% chord Max camber 4.9% at 40% chord Source UIUC Airfoil Coordinates Database
(goe575-il) GOE 575 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 575 airfoil Max thickness 13.3% at 29.8% chord Max camber 3.6% at 39.8% chord Source UIUC Airfoil Coordinates Database
(goe584-il) GOE 584 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 584 airfoil Max thickness 12.7% at 30% chord Max camber 5% at 40% chord Source UIUC Airfoil Coordinates Database
(goe585-il) GOE 585 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 585 airfoil Max thickness 8.2% at 20% chord Max camber 3.4% at 40% 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
(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
(goe591-il) GOE 591 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 591 airfoil Max thickness 11.2% at 30% chord Max camber 5.1% at 40% chord Source UIUC Airfoil Coordinates Database
(goe592-il) GOE 592 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 592 airfoil Max thickness 14.3% at 29.7% chord Max camber 7.5% at 39.7% chord Source UIUC Airfoil Coordinates Database

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