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.

(goe505-il) GOE 505 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 505 airfoil Max thickness 14% at 19.7% chord Max camber 5.9% at 39.7% chord Source UIUC Airfoil Coordinates Database
(goe417a-il) GOE 417A (GEW. PLATTE) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 417A (GEW. PLATTE) airfoil Max thickness 3.2% at 2.5% chord Max camber 5.9% at 40% 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
(goe499-il) GOE 499 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 499 airfoil Max thickness 6.8% at 30% chord Max camber 5.9% at 50% chord Source UIUC Airfoil Coordinates Database
(goe777-il) GOE 777 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 777 airfoil Max thickness 22% at 30% chord Max camber 5.9% at 30% chord Source UIUC Airfoil Coordinates Database
(goe529-il) GOE 529 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 529 airfoil Max thickness 9.7% at 29.9% chord Max camber 5.8% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe527-il) GOE 527 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 527 airfoil Max thickness 16.5% at 29.5% chord Max camber 5.8% at 39.5% chord Source UIUC Airfoil Coordinates Database
(goe319-il) GOE 319 (HANSA-BRANDENBURG II) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 319 (Hansa-Brandenburg II) airfoil Max thickness 10.3% at 29.8% chord Max camber 5.8% at 29.8% chord Source UIUC Airfoil Coordinates Database
(goe483-il) GOE 483 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 483 airfoil Max thickness 5.5% at 15% chord Max camber 5.8% at 40% 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

Page 19 of 164     9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28     Next

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