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.

(e341-il) EPPLER 341 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E341 flying wing airfoil Max thickness 13.9% at 32.8% chord Max camber 3% at 23.2% chord Source UIUC Airfoil Coordinates Database
(e642-il) EPPLER 642 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E642 sailplane airfoil Max thickness 15.1% at 39.4% chord Max camber 3% at 39.4% chord Source UIUC Airfoil Coordinates Database
(fx61168-il) FX 61-168 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 61-168 airfoil Max thickness 16.8% at 37.1% chord Max camber 3% at 37.1% chord Source UIUC Airfoil Coordinates Database
(goe113-il) GOE 113 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 113 airfoil Max thickness 6.7% at 30% chord Max camber 3% at 40% chord Source UIUC Airfoil Coordinates Database
(goe488-il) GOE 488 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 488 airfoil Max thickness 6.8% at 19.9% chord Max camber 3% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe587-il) GOE 587 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 587 airfoil Max thickness 5.8% at 40% chord Max camber 3% at 30% chord Source UIUC Airfoil Coordinates Database
(goe595-il) GOE 595 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 595 airfoil Max thickness 9.6% at 30% chord Max camber 3% at 40% chord Source UIUC Airfoil Coordinates Database
(goe683-il) GOE 683 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 683 airfoil Max thickness 19.9% at 30% chord Max camber 3% at 30% chord Source UIUC Airfoil Coordinates Database
(hq3010-il) HQ 3.0/10 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Quabeck HQ 3.0/10 R/C sailplane airfoil Max thickness 10% at 35% chord Max camber 3% at 50% chord Source UIUC Airfoil Coordinates Database
(hq3011-il) HQ 3.0/11 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Quabeck HQ 3.0/11 R/C sailplane airfoil Max thickness 11% at 35% chord Max camber 3% at 50% chord Source UIUC Airfoil Coordinates Database

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