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.

(m16-il) NACA M16 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA/Munk M-16 airfoil Max thickness 6.2% at 30% chord Max camber 4.1% at 30% chord Max Cl/Cd 102.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e1213-il) EPPLER 1213 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E1213 general aviation airfoil Max thickness 17.4% at 22.1% chord Max camber 2.1% at 35.1% chord Max Cl/Cd 102.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(v43012-il) BOEING VERTOL V43012-1.58 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Boeing-Vertol V43012-1.58 rotorcraft airfoil Max thickness 12% at 32% chord Max camber 3.7% at 15% chord Max Cl/Cd 102.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(goe738-il) GOE 738 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 738 airfoil Max thickness 15.4% at 30% chord Max camber 2.1% at 30% chord Max Cl/Cd 102.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(sd2083-il) SD2083 (9.0%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig/Donovan SD2083 low Reynolds number airfoil Max thickness 9% at 35.2% chord Max camber 2.5% at 49.6% chord Max Cl/Cd 102.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database

(e224-il) E224 (10.17%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E224 low Reynolds number airfoil Max thickness 10.2% at 29.8% chord Max camber 1.5% at 54.2% chord Max Cl/Cd 102.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(hq3512-il) HQ 3.5/12 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Quabeck HQ 3.5/12 R/C sailplane airfoil Max thickness 12% at 35% chord Max camber 3.5% at 50% chord Max Cl/Cd 102.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(fx60160-il) FX 60-160 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Wortmann FX 60-160 airfoil Max thickness 15.6% at 40% chord Max camber 3.1% at 60% chord Max Cl/Cd 102.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(e341-il) EPPLER 341 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E341 flying wing airfoil Max thickness 13.9% at 32.8% chord Max camber 3% at 23.2% chord Max Cl/Cd 102.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database
(s5010-il) S5010		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Selig S5010 low Reynolds number airfoil Max thickness 9.8% at 27.6% chord Max camber 1.8% at 32% chord Max Cl/Cd 102.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database