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.

(nacacyh-il) NACA CYH		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA CYH airfoil Max thickness 11.7% at 30% chord Max camber 2.8% at 40% chord Max Cl/Cd 64.7 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(e221-il) E221 (9.39%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E221 low Reynolds number airfoil Max thickness 9.4% at 28.1% chord Max camber 1.6% at 32.6% chord Max Cl/Cd 64.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(mh20-il) MH 20 9.01%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 20 for F3D Pylon Racing Max thickness 9% at 32.2% chord Max camber 1.9% at 37.3% chord Max Cl/Cd 64.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe711-il) GOE 711 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 711 airfoil Max thickness 14.9% at 30% chord Max camber 6.3% at 30% chord Max Cl/Cd 64.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(e343-il) EPPLER 343 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E343 flying wing airfoil Max thickness 14.5% at 30.9% chord Max camber 4% at 26% chord Max Cl/Cd 64.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database

(n24-il) N-24		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	N-24 airfoil Max thickness 17% at 30% chord Max camber 5.4% at 40% chord Max Cl/Cd 64.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(s1223rtl-il) S1223 RTL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Richard T. LaSalle modification of the S1223 to S1223RTL Max thickness 13.5% at 19.9% chord Max camber 8.3% at 55.2% chord Max Cl/Cd 64.6 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(goe655-il) GOE 655 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 655 airfoil Max thickness 13.9% at 30% chord Max camber 4.4% at 40% chord Max Cl/Cd 64.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(fx05188-il) WORTMANN FX 05-188 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 05-188 airfoil Max thickness 18.8% at 37.1% chord Max camber 2.6% at 50% chord Max Cl/Cd 64.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database
(fxs03182-il) FX S 03-182 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX S 03-182 airfoil Max thickness 18.2% at 40.2% chord Max camber 2.9% at 56.5% chord Max Cl/Cd 64.5 at Re# 200,000 Source UIUC Airfoil Coordinates Database