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.

(goe648-il) GOE 648 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 648 airfoil Max thickness 15.2% at 29.4% chord Max camber 3.9% at 39.4% chord Source UIUC Airfoil Coordinates Database
(goe650-il) GOE 650 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 650 airfoil Max thickness 13.4% at 19.5% chord Max camber 4.4% at 49.5% chord Source UIUC Airfoil Coordinates Database
(goe652-il) GOE 652 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 652 airfoil Max thickness 17.1% at 20% chord Max camber 9.3% at 50% chord Source UIUC Airfoil Coordinates Database
(goe654-il) GOE 654 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 654 airfoil Max thickness 14.5% at 30% chord Max camber 5.2% at 40% chord Source UIUC Airfoil Coordinates Database
(goe655-il) GOE 655 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 655 airfoil Max thickness 13.9% at 30% chord Max camber 4.4% at 40% chord Source UIUC Airfoil Coordinates Database
(goe670-il) GOE 670 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 670 airfoil Max thickness 9% at 30% chord Max camber 3.4% at 40% chord Source UIUC Airfoil Coordinates Database
(goe673-il) GOE 673 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 673 airfoil Max thickness 10.8% at 29.7% chord Max camber 2.8% at 49.7% chord Source UIUC Airfoil Coordinates Database
(goe675-il) GOE 675 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 675 airfoil Max thickness 14.9% at 29.5% chord Max camber 5.9% at 39.5% chord Source UIUC Airfoil Coordinates Database
(goe676-il) GOE 676 (= M 12) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 676 (= M 12) airfoil Max thickness 11.9% at 30% chord Max camber 2% at 30% chord Source UIUC Airfoil Coordinates Database
(goe677-il) GOE 677 (= M 6) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 677 (= M 6) airfoil Max thickness 12% at 30% chord Max camber 2.2% at 30% chord Source UIUC Airfoil Coordinates Database

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