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.

(usa46-il) USA 46 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	USA-46 airfoil Max thickness 6.5% at 20% chord Max camber 2.2% at 40% chord Source UIUC Airfoil Coordinates Database
(ag04-il) AG04		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Drela AG04 airfoil Max thickness 6.4% at 22.5% chord Max camber 1.7% at 41.5% chord Source UIUC Airfoil Coordinates Database
(goe264-il) GOE 264 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 264 airfoil Max thickness 6.4% at 20.2% chord Max camber 5.7% at 28.9% chord Source UIUC Airfoil Coordinates Database
(goe381-il) GOE 381 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 381 airfoil Max thickness 6.4% at 30% chord Max camber 5.8% at 30% chord Source UIUC Airfoil Coordinates Database
(goe445-il) GOE 445 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 445 airfoil Max thickness 6.4% at 40% chord Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database
(usa5-il) USA 5 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	USA-5 airfoil Max thickness 6.4% at 30% chord Max camber 4.5% at 40% chord Source UIUC Airfoil Coordinates Database
(e471-il) E471 (6.25%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E471 airfoil Max thickness 6.3% at 29.8% chord Max camber 4.5% at 53.5% chord Source UIUC Airfoil Coordinates Database
(goe484-il) GOE 484 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 484 airfoil Max thickness 6.3% at 30% chord Max camber 5% at 50% chord Source UIUC Airfoil Coordinates Database
(goe57-il) GOE 57 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 57 airfoil Max thickness 6.3% at 19.9% chord Max camber 5.1% at 39.9% chord Source UIUC Airfoil Coordinates Database
(goe803h-il) GOE 803 (HACKLINGER) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 803 (Hacklinger) airfoil Max thickness 6.3% at 15% chord Max camber 6.6% at 40% chord Source UIUC Airfoil Coordinates Database

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