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.

(mh94-il) MH 94 16.03%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 94 parafoil Max thickness 16% at 34.1% chord Max camber 1.3% at 74.1% chord Source UIUC Airfoil Coordinates Database
(mh95-il) MH 95 15.86%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 95 parafoil Max thickness 15.8% at 33.6% chord Max camber 0.9% at 81.6% chord Source UIUC Airfoil Coordinates Database
(mh33-il) MH33		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 33 for F3E and F3B Max thickness 7.3% at 29.3% chord Max camber 1.1% at 43.9% chord Source UIUC Airfoil Coordinates Database
(miley-il) MILEY M06-13-128		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Miley MO6-13-128 airfoil Max thickness 12.9% at 35% chord Max camber 4.9% at 35% chord Source UIUC Airfoil Coordinates Database
(mrc-16-il) MRC-16		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Drela MRC-16 Max thickness 13.9% at 34.6% chord Max camber 3% at 40.3% chord Source UIUC Airfoil Coordinates Database
(mrc-20-il) MRC-20		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Drela MRC-20 Max thickness 15.6% at 38.2% chord Max camber 2.9% at 48% chord Source UIUC Airfoil Coordinates Database
(mue139-il) MUE 139		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	MUE 139 airfoil Max thickness 13.9% at 22.2% chord Max camber 4.7% at 30.9% chord Source UIUC Airfoil Coordinates Database
(n10-il) N-10		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	N-10 airfoil Max thickness 11.2% at 30% chord Max camber 3.6% at 40% chord Source UIUC Airfoil Coordinates Database
(n11-il) N-11		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	N-11 airfoil Max thickness 10.9% at 30% chord Max camber 4.4% at 40% chord Source UIUC Airfoil Coordinates Database
(n12-il) N-12		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	N-12 airfoil Max thickness 10.5% at 30% chord Max camber 0.2% at 15% chord Source UIUC Airfoil Coordinates Database

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