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.

(goe395-il) GOE 395 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 395 airfoil Max thickness 6.1% at 19.9% chord Max camber 7% at 49.9% chord Source UIUC Airfoil Coordinates Database
(goe396-il) GOE 396 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 396 airfoil Max thickness 4.7% at 30% chord Max camber 5.8% at 40% chord Source UIUC Airfoil Coordinates Database
(goe397-il) GOE 397 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 397 airfoil Max thickness 5.1% at 30% chord Max camber 4% at 40% chord Source UIUC Airfoil Coordinates Database
(goe398-il) GOE 398 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 398 airfoil Max thickness 13.9% at 30% chord Max camber 4.9% at 40% chord Source UIUC Airfoil Coordinates Database
(goe399-il) GOE 399 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 399 airfoil Max thickness 6.9% at 29.9% chord Max camber 4.2% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe400-il) GOE 400 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 400 airfoil Max thickness 6.1% at 20% chord Max camber 4.9% at 40% chord Source UIUC Airfoil Coordinates Database
(goe401-il) GOE 401 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 401 airfoil Max thickness 7.1% at 29.9% chord Max camber 4.9% at 29.9% chord Source UIUC Airfoil Coordinates Database
(goe402-il) GOE 402 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 402 airfoil Max thickness 6.8% at 20% chord Max camber 5.7% at 30% chord Source UIUC Airfoil Coordinates Database
(goe403-il) GOE 403 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 403 airfoil Max thickness 6.7% at 29.9% chord Max camber 4.3% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe404-il) GOE 404 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 404 airfoil Max thickness 13.2% at 29.6% chord Max camber 5% at 29.6% chord Source UIUC Airfoil Coordinates Database

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