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.

(fx73cl2152-il) FX 73-CL2-152		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 73-CL2-152 airfoil Max thickness 15.2% at 22.2% chord Max camber 6.6% at 43.5% chord Max Cl/Cd 135.3 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe497-il) GOE 497 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 497 airfoil Max thickness 12.7% at 30% chord Max camber 5.3% at 50% chord Max Cl/Cd 135.2 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e655-il) EPPLER 655 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E655 sailplane airfoil Max thickness 17.3% at 37.3% chord Max camber 3.9% at 42.4% chord Max Cl/Cd 135.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(fx84w175-il) FX 84-W-175		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 84-W-175 airfoil for use on wind turbines (W) Max thickness 17.6% at 37.1% chord Max camber 4.4% at 43.5% chord Max Cl/Cd 135.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(s1221-il) S1221 w/o flap		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig S1221 airfoil Max thickness 12.1% at 21.8% chord Max camber 4.9% at 49.1% chord Max Cl/Cd 135.1 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database

(r1082t-il) RONCZ 1082T VOYAGER TIP OUTER AFT WING AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Roncz 1082T Voyager tip outer aft wing airfoil Max thickness 16% at 40% chord Max camber 3% at 40% chord Max Cl/Cd 135 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe233-il) GOE 233 (MVA CA4) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 233 (MVA CA4) airfoil Max thickness 11.6% at 19.8% chord Max camber 8.2% at 49.8% chord Max Cl/Cd 134.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(fx75141-il) WORTMANN FX 75-141		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 75-141 airfoil Max thickness 14.1% at 37.1% chord Max camber 3.4% at 53.3% chord Max Cl/Cd 134.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(naca652415a05-il) NACA 65(2)-415 a=0.5		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 65(2)-415 a=0.5 airfoil Max thickness 15% at 39.9% chord Max camber 3% at 45% chord Max Cl/Cd 134.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(raf32-il) RAF 32 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	RAF-32 airfoil Max thickness 12.7% at 30% chord Max camber 5% at 50% chord Max Cl/Cd 134.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database