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.

(goe308-il) GOE 308 (MVA H.40) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 308 (MVA H.40) airfoil Max thickness 8.1% at 29.9% chord Max camber 5% at 29.9% chord Source UIUC Airfoil Coordinates Database
(usa27m2-il) USA 27 mod. AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	USA-27MOD airfoil Max thickness 13.3% at 30% chord Max camber 5% at 40% chord Source UIUC Airfoil Coordinates Database
(goe746-il) GOE 746 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 746 airfoil Max thickness 9.8% at 30% chord Max camber 5% at 30% chord Source UIUC Airfoil Coordinates Database
(raf32-il) RAF 32 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	RAF-32 airfoil Max thickness 12.7% at 30% chord Max camber 5% at 50% chord Source UIUC Airfoil Coordinates Database
(sg6043-il) SG6043		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig / Giguere SG6043 wind turbine airfoil (high L/D) Max thickness 10% at 32.1% chord Max camber 5.1% at 53.3% 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
(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
(goe412-il) GOE 412 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 412 airfoil Max thickness 13.1% at 29.7% chord Max camber 5.1% at 39.7% chord Source UIUC Airfoil Coordinates Database
(goe530-il) GOE 530 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 530 airfoil Max thickness 12.9% at 29.8% chord Max camber 5.1% at 29.8% chord Source UIUC Airfoil Coordinates Database
(goe702-il) GOE 702 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 702 airfoil Max thickness 16.6% at 19.4% chord Max camber 5.1% at 39.4% chord Source UIUC Airfoil Coordinates Database

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