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.

(goe371-il) GOE 371 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 371 airfoil Max thickness 7% at 29.9% chord Max camber 4.6% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe372-il) GOE 372 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 372 airfoil Max thickness 6.2% at 29.9% chord Max camber 4.3% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe373-il) GOE 373 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 373 airfoil Max thickness 6.5% at 29.9% chord Max camber 5.1% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe374-il) GOE 374 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 374 airfoil Max thickness 6.5% at 30% chord Max camber 4.5% at 30% chord Source UIUC Airfoil Coordinates Database
(goe375-il) GOE 375 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 375 airfoil Max thickness 6.5% at 20% chord Max camber 4.5% at 30% chord Source UIUC Airfoil Coordinates Database
(goe376-il) GOE 376 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 376 airfoil Max thickness 6.6% at 30% chord Max camber 5% at 30% chord Source UIUC Airfoil Coordinates Database
(goe377-il) GOE 377 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 377 airfoil Max thickness 6.5% at 30% chord Max camber 3.9% at 40% chord Source UIUC Airfoil Coordinates Database
(goe379-il) GOE 379 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 379 airfoil Max thickness 6.5% at 30% chord Max camber 5.2% at 40% chord Source UIUC Airfoil Coordinates Database
(goe380-il) GOE 380 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 380 airfoil Max thickness 6.6% at 30% chord Max camber 5.6% at 30% chord Source UIUC Airfoil Coordinates Database
(goe381-il) GOE 381 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 381 airfoil Max thickness 6.4% at 30% chord Max camber 5.8% at 30% chord Source UIUC Airfoil Coordinates Database

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