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.

(marsden-il) Marsden		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Marsden airfoil Max thickness 27.9% at 31.6% chord Max camber 7.7% at 37.6% chord Max Cl/Cd 5.1 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(kenmar-il) KENNEDY AND MARSDEN AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	University of Alberta/Kennedy and Marsden high lift airfoil Max thickness 27.9% at 31% chord Max camber 7.7% at 36.9% chord Max Cl/Cd 5.1 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(ua79sff-il) UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	University of Alberta/Marsden UA 79-SF-187 sailplane airfoil FLAP Max thickness 8.7% at 73.1% chord Max camber 3.4% at 78.1% chord Max Cl/Cd 3.8 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(fx77w343-il) WORTMANN FX 77-W-343 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 77-W-343 wind turbine airfoil Max thickness 34.4% at 33.9% chord Max camber 4.7% at 25% chord Max Cl/Cd 3.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(bacj-il) BOEING AIRFOIL J (no closed TE)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Boeing Commercial Airplane Company airfoil J Max thickness 10.1% at 40% chord Max camber 1.7% at 78% chord Max Cl/Cd -1 at Re# 200,000 Source UIUC Airfoil Coordinates Database

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