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.

(goe447-il) GOE 447 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 447 airfoil Max thickness 12.7% at 29.7% chord Max camber 8% at 39.7% chord Source UIUC Airfoil Coordinates Database
(goe448-il) GOE 448 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 448 airfoil Max thickness 12.9% at 29.8% chord Max camber 10.5% at 39.8% chord Source UIUC Airfoil Coordinates Database
(goe449-il) GOE 449 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 449 airfoil Max thickness 17% at 30% chord Max camber 5.4% at 40% chord Source UIUC Airfoil Coordinates Database
(goe450-il) GOE 450 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 450 airfoil Max thickness 8.9% at 29.9% chord Max camber 5.2% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe451-il) GOE 451 AIRFOIL (modified line 6)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 451 airfoil Max thickness 4.4% at 30% chord Max camber 5.6% at 40% chord Source UIUC Airfoil Coordinates Database
(goe456-il) GOE 456 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 456 airfoil Max thickness 7.2% at 29.9% chord Max camber 5.2% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe457-il) GOE 457 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 457 airfoil Max thickness 7.8% at 19.9% chord Max camber 4.2% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe458-il) GOE 458 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 458 airfoil Max thickness 7.2% at 29.9% chord Max camber 5.2% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe459-il) GOE 459 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 459 airfoil Max thickness 12.7% at 30% chord Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database
(goe460-il) GOE 460 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 460 airfoil Max thickness 20.5% at 30% chord Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database

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