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.

(goe620-il) GOE 620 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 620 airfoil Max thickness 17.5% at 30% chord Max camber 5.9% at 50% chord Source UIUC Airfoil Coordinates Database
(goe621-il) GOE 621 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 621 airfoil Max thickness 15% at 29.5% chord Max camber 5% at 49.5% chord Source UIUC Airfoil Coordinates Database
(goe622-il) GOE 622 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 622 airfoil Max thickness 8% at 30% chord Max camber 2.4% at 40% chord Source UIUC Airfoil Coordinates Database
(goe623-il) GOE 623 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 623 airfoil Max thickness 12% at 30% chord Max camber 3.8% at 40% chord Source UIUC Airfoil Coordinates Database
(goe624-il) GOE 624 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 624 airfoil Max thickness 16% at 30% chord Max camber 5.2% at 40% chord Source UIUC Airfoil Coordinates Database
(goe625-il) GOE 625 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 625 airfoil Max thickness 20% at 30% chord Max camber 6.1% at 40% chord Source UIUC Airfoil Coordinates Database
(goe626-il) GOE 626 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 626 airfoil Max thickness 16.5% at 19.3% chord Max camber 5.1% at 49.3% chord Source UIUC Airfoil Coordinates Database
(goe627-il) GOE 627 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 627 airfoil Max thickness 15.8% at 30% chord Max camber 4.1% at 30% chord Source UIUC Airfoil Coordinates Database
(goe628-il) GOE 628 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 628 airfoil Max thickness 16.7% at 19.4% chord Max camber 5.6% at 39.3% chord Source UIUC Airfoil Coordinates Database
(goe629-il) GOE 629 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 629 airfoil Max thickness 13.6% at 29.4% chord Max camber 2.8% at 39.4% chord Source UIUC Airfoil Coordinates Database

Page 83 of 164     73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92     Next

Please see the source web site or designer for any license conditions.