Airfoil Tools
Search 1638 airfoils

You have 0 airfoils loaded.
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.

(goe342-il) GOE 342 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 342 airfoil Max thickness 5.4% at 20% chord Max camber 6.2% at 40% chord Max Cl/Cd 47.8 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(e62-il) E62 (5.62%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E62 low Reynolds number airfoil Max thickness 5.6% at 26.2% chord Max camber 5% at 49.3% chord Max Cl/Cd 47.7 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(ah6407-il) AH-6-40-7 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Althaus AH 6-407 airfoil Max thickness 6.9% at 20% chord Max camber 5.5% at 40% chord Max Cl/Cd 46.9 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(e61-il) E61 (5.64%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E61 low Reynolds number airfoil Max thickness 5.7% at 23.8% chord Max camber 6.4% at 51% chord Max Cl/Cd 46.9 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(e471-il) E471 (6.25%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E471 airfoil Max thickness 6.3% at 29.8% chord Max camber 4.5% at 53.5% chord Max Cl/Cd 46.8 at Re# 50,000 Source UIUC Airfoil Coordinates Database

(bw3-il) Bergey BW-3 (smoothed)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Bergey BW-3 wind turbine airfoil (smoothed) Max thickness 5% at 7.4% chord Max camber 5.7% at 45.4% chord Max Cl/Cd 46.7 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe417a-il) GOE 417A (GEW. PLATTE) AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 417A (GEW. PLATTE) airfoil Max thickness 3.2% at 2.5% chord Max camber 5.9% at 40% chord Max Cl/Cd 46.5 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(goe427-il) GOE 427 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 427 airfoil Max thickness 4.6% at 20% chord Max camber 5.4% at 40% chord Max Cl/Cd 46.5 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(e471-il) E471 (6.25%)		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E471 airfoil Max thickness 6.3% at 29.8% chord Max camber 4.5% at 53.5% chord Max Cl/Cd 46.4 at Re# 50,000 Source UIUC Airfoil Coordinates Database
(e59-il) EPPLER 59 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Eppler E59 low Reynolds number airfoil Max thickness 5.6% at 25% chord Max camber 5.2% at 50% chord Max Cl/Cd 46.2 at Re# 50,000 Source UIUC Airfoil Coordinates Database