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.

(ah79100b-il) AH 79-100 B AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 79-100B airfoil Max thickness 10% at 30.9% chord Max camber 6.4% at 50% chord Source UIUC Airfoil Coordinates Database
(sokolov-il) SOKOLOV AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Sokolov R/C sailplane airfoil Max thickness 7.1% at 25% chord Max camber 6.3% at 50% chord Source UIUC Airfoil Coordinates Database
(m24-il) NACA M24 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA/Munk M-24 airfoil Max thickness 12% at 30.1% chord Max camber 6.3% at 30.1% chord Source UIUC Airfoil Coordinates Database
(m22-il) NACA M22 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA/Munk M-22 airfoil Max thickness 6.3% at 30% chord Max camber 6.3% at 30% chord Source UIUC Airfoil Coordinates Database
(goe81-il) GOE 81 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 81 airfoil Max thickness 7.4% at 29.9% chord Max camber 6.3% at 29.9% chord Source UIUC Airfoil Coordinates Database
(goe804-il) GOE 804 (EA 8) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 804 (EA 8) airfoil Max thickness 6% at 40% chord Max camber 6.3% at 50% chord Source UIUC Airfoil Coordinates Database
(goe711-il) GOE 711 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 711 airfoil Max thickness 14.9% at 30% chord Max camber 6.3% at 30% chord Source UIUC Airfoil Coordinates Database
(goe562-il) GOE 562 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 562 airfoil Max thickness 14.1% at 30% chord Max camber 6.3% at 30% 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
(goe446-il) GOE 446 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 446 airfoil Max thickness 12.9% at 29.7% chord Max camber 6.3% at 39.7% chord Source UIUC Airfoil Coordinates Database

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