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.

(goe116-il) GOE 116 (MVA MK.3) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 116 (MVA MK.3) airfoil Max thickness 9.3% at 39.8% chord Max camber 4.1% at 39.8% chord Source UIUC Airfoil Coordinates Database
(mh116-il) MH 116 9.84%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 116 for a propeller for ultralight Max thickness 9.9% at 32.4% chord Max camber 4.1% at 46.4% chord Source UIUC Airfoil Coordinates Database
(nacam18-il) NACA M18		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA M18 airfoil Max thickness 12% at 30% chord Max camber 4.1% at 30% chord Source UIUC Airfoil Coordinates Database
(goe408-il) GOE 408 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 408 airfoil Max thickness 7.8% at 30% chord Max camber 4.1% at 30% chord Source UIUC Airfoil Coordinates Database
(goe593-il) GOE 593 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 593 airfoil Max thickness 11.9% at 30% chord Max camber 4.1% at 40% chord Source UIUC Airfoil Coordinates Database
(goe526-il) GOE 526 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 526 airfoil Max thickness 12.3% at 29.7% chord Max camber 4.1% at 39.7% chord Source UIUC Airfoil Coordinates Database
(goe16k-il) GOE 16K AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 16K airfoil Max thickness 18.2% at 50% chord Max camber 4.1% at 50% chord Source UIUC Airfoil Coordinates Database
(goe257-il) GOE 257 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 257 airfoil Max thickness 8.8% at 30% chord Max camber 4.1% at 30% chord Source UIUC Airfoil Coordinates Database
(usa45-il) USA 45 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	USA-45 airfoil Max thickness 14.5% at 29.8% chord Max camber 4.1% at 29.8% chord Source UIUC Airfoil Coordinates Database
(goe315-il) GOE 315 (HANSA-BRANDENBURG III.5) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 315 (Hansa-Brandenburg III.5) airfoil Max thickness 8.1% at 29.9% chord Max camber 4.1% at 29.9% chord Source UIUC Airfoil Coordinates Database

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