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.

(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
(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
(goe54-il) GOE 54 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 54 airfoil Max thickness 6.5% at 14.9% chord Max camber 3.5% at 19.9% chord Source UIUC Airfoil Coordinates Database
(goe598-il) GOE 598 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 598 airfoil Max thickness 6.5% at 39.8% chord Max camber 1% at 49.8% chord Source UIUC Airfoil Coordinates Database
(ht23-il) HT23		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Drela HT23 airfoil Max thickness 6.5% at 20.8% chord Max camber 1.1% at 22.6% chord Source UIUC Airfoil Coordinates Database
(raf15-il) RAF 15 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	RAF-15 airfoil Max thickness 6.5% at 15% chord Max camber 2.6% at 30% chord Source UIUC Airfoil Coordinates Database
(raf25-il) RAF 25 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	RAF-25 airfoil Max thickness 6.5% at 29.9% chord Max camber 1% at 49.9% chord Source UIUC Airfoil Coordinates Database

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