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.

(goe493-il) GOE 493 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 493 airfoil Max thickness 14.9% at 29.3% chord Max camber 3.4% at 49.3% chord Source UIUC Airfoil Coordinates Database
(goe494-il) GOE 494 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 494 airfoil Max thickness 5% at 20% chord Max camber 5.1% at 50% chord Source UIUC Airfoil Coordinates Database
(goe495-il) GOE 495 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 495 airfoil Max thickness 6.9% at 30% chord Max camber 5% at 50% chord Source UIUC Airfoil Coordinates Database
(goe496-il) GOE 496 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 496 airfoil Max thickness 10% at 30% chord Max camber 5% at 50% chord Source UIUC Airfoil Coordinates Database
(goe497-il) GOE 497 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 497 airfoil Max thickness 12.7% at 30% chord Max camber 5.3% at 50% chord Source UIUC Airfoil Coordinates Database
(goe498-il) GOE 498 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 498 airfoil Max thickness 15.9% at 29.4% chord Max camber 5.5% at 49.4% 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
(goe500-il) GOE 500 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 500 airfoil Max thickness 10% at 30% chord Max camber 6% at 50% chord Source UIUC Airfoil Coordinates Database
(goe501-il) GOE 501 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 501 airfoil Max thickness 12.8% at 30% chord Max camber 6.3% at 50% chord Source UIUC Airfoil Coordinates Database
(goe502-il) GOE 502 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 502 airfoil Max thickness 15.9% at 29.3% chord Max camber 6.1% at 49.4% chord Source UIUC Airfoil Coordinates Database

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