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.

(ah93w257-il) AH 93-W-257		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 93-W-257 airfoil for use on wind turbines (W) Max thickness 25.7% at 30.9% chord Max camber 2.1% at 77.8% chord Max Cl/Cd 92.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(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 92.7 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(naca747a415-il) NACA 747A415		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	NACA 747A415 airfoil Max thickness 15% at 40.2% chord Max camber 3% at 35% chord Max Cl/Cd 92.6 at Re# 500,000 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 92.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(daytonwright6-il) Dayton-Wright 6		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Dayton-Wright 6 airfoil Max thickness 13.6% at 30% chord Max camber 4.9% at 40% chord Max Cl/Cd 92.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database

(mh104-il) MH 104 15.28%		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Martin Hepperle MH 104 for stall controlled wind turbines Max thickness 15.2% at 26.4% chord Max camber 1.9% at 31.1% chord Max Cl/Cd 92.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e642-il) EPPLER 642 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E642 sailplane airfoil Max thickness 15.1% at 39.4% chord Max camber 3% at 39.4% chord Max Cl/Cd 92.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(goe256-il) GOE 256 (JUNKERS E) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 256 (JUNKERS E) airfoil Max thickness 16% at 29.6% chord Max camber 4.7% at 39.6% chord Max Cl/Cd 92.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(e337-il) EPPLER 337 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E337 flying wing airfoil Max thickness 13.1% at 32% chord Max camber 3.2% at 22.4% chord Max Cl/Cd 92.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
(hq3011-il) HQ 3.0/11 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Quabeck HQ 3.0/11 R/C sailplane airfoil Max thickness 11% at 35% chord Max camber 3% at 50% chord Max Cl/Cd 92.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database