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.

(goe628-il) GOE 628 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 628 airfoil Max thickness 16.7% at 19.4% chord Max camber 5.6% at 39.3% chord Source UIUC Airfoil Coordinates Database
(goe512-il) GOE 512 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 512 airfoil Max thickness 13.9% at 19.9% chord Max camber 5.6% at 29.9% chord Source UIUC Airfoil Coordinates Database
(goe508-il) GOE 508 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 508 airfoil Max thickness 16.5% at 30% chord Max camber 5.6% at 40% chord Source UIUC Airfoil Coordinates Database
(goe358-il) GOE 358 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 358 airfoil Max thickness 10.9% at 20% chord Max camber 5.6% at 50% chord Source UIUC Airfoil Coordinates Database
(fx73170a-il) WORTMANN FX 73-170 A		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 73-170 A airfoil Max thickness 17.1% at 43.5% chord Max camber 5.6% at 43.5% chord Source UIUC Airfoil Coordinates Database
(goe615-il) GOE 615 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 615 airfoil Max thickness 13.7% at 29.7% chord Max camber 5.6% at 39.7% chord Source UIUC Airfoil Coordinates Database
(goe451-il) GOE 451 AIRFOIL (modified line 6)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 451 airfoil Max thickness 4.4% at 30% chord Max camber 5.6% at 40% chord Source UIUC Airfoil Coordinates Database
(goe124-il) GOE 124 (MVA H.4) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 124 (MVA H.4) airfoil Max thickness 7.9% at 29.9% chord Max camber 5.6% at 39.9% chord Source UIUC Airfoil Coordinates Database
(fx69pr281-il) FX 69-PR-281		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 69-PR-281 airfoil Max thickness 28.1% at 22.2% chord Max camber 5.6% at 50% 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

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