Airfoil Tools
Search 1638 airfoils

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Your Reynold number range is 50,000 to 1,000,000. (set)

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.

(fx76mp160-il) FX 76-MP-160		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 76-MP-160 airfoil Max thickness 16.1% at 33.9% chord Max camber 6.1% at 50% chord Source UIUC Airfoil Coordinates Database
(fx83w160-il) FX 83-W-160		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 83-W-160 airfoil for use on wind turbines (W) Max thickness 16.1% at 37.1% chord Max camber 3.9% at 62.9% chord Source UIUC Airfoil Coordinates Database
(goe410-il) GOE 410 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 410 airfoil Max thickness 16.1% at 30% chord Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database
(goe535-il) GOE 535 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 535 airfoil Max thickness 16.1% at 20% chord Max camber 5.8% at 50% chord Source UIUC Airfoil Coordinates Database
(goe692-il) GOE 692 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 692 airfoil Max thickness 16.1% at 30% chord Max camber 5% at 40% chord Source UIUC Airfoil Coordinates Database

(doa5-il) DORNIER A-5 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Dornier A-5 airfoil (reconstruction) (DO 228 wing) Max thickness 16.2% at 40.1% chord Max camber 2.5% at 76% chord Source UIUC Airfoil Coordinates Database
(e435-il) EPPLER 435 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E435 sailplane airfoil Max thickness 16.2% at 40.9% chord Max camber 4.4% at 56.2% chord Source UIUC Airfoil Coordinates Database
(e473-il) EPPLER 473 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E473 aerobatic aircraft airfoil Max thickness 16.2% at 21.2% chord Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database
(e546-il) EPPLER 546 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E546 general aviation airfoil Max thickness 16.2% at 40.3% chord Max camber 1.8% at 26.2% chord Source UIUC Airfoil Coordinates Database
(e656-il) EPPLER 656 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E656 sailplane airfoil Max thickness 16.2% at 37% chord Max camber 4.8% at 42.2% chord Source UIUC Airfoil Coordinates Database